Publications

2021

  1. Multipoint Aerodynamic Shape Optimization for Subsonic and Supersonic Regimes

    M. Mangano, and J. R. R. A. Martins

    Journal of Aircraft, 2021

    doi:10.2514/1.C036216

    Details
  2. A Surface Mesh Warping Method Near Component Intersections for High-Fidelity Design Optimization

    A. Yildirim, C. A. Mader, and J. R. R. A. Martins

    Engineering with Computers, 2021

    doi:10.1007/s00366-020-01247-w

    Details
  3. Enabling Large-scale Multidisciplinary Design Optimization through Adjoint Sensitivity Analysis

    J. R. R. A. Martins, and G. J. Kennedy

    Structural and Multidisciplinary Optimization, 2021

    Details
  4. Rapid Airfoil Design Optimization via Neural Networks-based Parameterization and Surrogate Modeling

    X. Du, P. He, and J. R. R. A. Martins

    Aerospace Science and Technology, 113106701, 2021

    doi:10.1016/j.ast.2021.106701

    Details
  5. Enabling Large-scale Multidisciplinary Design Optimization through Adjoint Sensitivity Analysis

    J. R. R. A. Martins, and G. Kennedy

    Structural and Multidisciplinary Optimization, 2021

    Details
  6. Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization

    N. Secco, G. K. W. Kenway, P. He, C. A. Mader, and J. R. R. A. Martins

    AIAA Journal, 59(4):1151–1168, 2021

    doi:10.2514/1.J059491

    Details
  7. The DIRECT Algorithm—25 Years Later

    D. R. Jones, and J. R. R. A. Martins

    Journal of Global Optimization, 79521–566, 2021

    doi:10.1007/s10898-020-00952-6

    Details
  8. 3-D High-Fidelity Hydrostructural Optimization of Cavitation-Free Composite Lifting Surfaces

    Y. Liao, J. R. R. A. Martins, and Y. L. Young

    Composite Structures, 2021

    Details
  9. Coupled Newton–Krylov Time-Spectral Solver for Flutter and Limit Cycle Oscillation Prediction

    S. He, E. Jonsson, C. A. Mader, and J. R. R. A. Martins

    AIAA Journal, 59(6):2214–2232, 2021

    doi:10.2514/1.J059224

    Details
  10. An MDO-Based Methodology for Static Aeroelastic Scaling of Wings Under Non-Similar Flow

    J. M. Colomer, N. Bartoli, T. Lefebvre, J. R. R. A. Martins, and J. Morlier

    Structural and Multidisciplinary Optimization, 631045–1061, 2021

    doi:10.1007/s00158-020-02804-z

    Details
  11. Truss topology design optimization with guaranteed kinematic stability

    M. Shahabsafa, R. Fakhimi, W. Lei, S. He, L. Zuluaga, J. R. R. A. Martins, and T. Terlaky

    Structural and Multidisciplinary Optimization, 6321–38, 2021

    doi:10.1007/s00158-020-02698-x

    Details
  12. Natural Laminar Flow Wing Optimization Using a Discrete Adjoint Approach

    Y. Shi, C. A. Mader, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 64541—562, 2021

    doi:10.1007/s00158-021-02936-w

    Details
  13. RANS-Based Aerodynamic Shape Optimization of a Wing Considering Propeller-Wing Interaction

    S. Chauhan, and J. R. R. A. Martins

    Journal of Aircraft, 58(3):497–513, 2021

    doi:10.2514/1.C035991

    Details
  14. Discrete Multi-Scenario Truss Sizing Optimization: Model Analysis and Computational Experiments

    R. Fakhimi, M. Shahabsafa, W. Lei, S. He, J. R. R. A. Martins, T. Terlaky, and L. F. Zuluaga

    Structural and Multidisciplinary Optimization, 2021

    Details

2020

  1. Toward Automatic PSE-based Transition to Turbulence Prediction for Aerodynamic Flows

    G. L. O. Halila, K. Fidkowski, and J. R. R. A. Martins

    AIAA Journal, 2020

    doi:10.2514/1.J059516

    Details
  2. Adjoint-Based Aerodynamic Shape Optimization Including Transition to Turbulence Effects

    G. L. O. Halila, J. R. R. A. Martins, and K. J. Fidkowski

    Aerospace Science and Technology, (107):1–15, 2020

    doi:10.1016/j.ast.2020.106243

    Details
  3. Efficient Aerodynamic Shape Optimization with Deep-learning-based Filtering

    J. Li, M. Zhang, J. R. R. A. Martins, and C. Shu

    AIAA Journal, 58(10):4243–4259, 2020

    doi:10.2514/1.J059254

    Details
  4. ADflow: An open-source computational fluid dynamics solver for aerodynamic and multidisciplinary optimization

    C. A. Mader, G. K. W. Kenway, A. Yildirim, and J. R. R. A. Martins

    Journal of Aerospace Information Systems, 17(9):508–527, 2020

    doi:10.2514/1.I010796

    Details
  5. Coupled Aeropropulsive Design Optimization of a Three-Dimensional BLI Propulsor Considering Inlet Distortion

    J. S. Gray, C. A. Mader, G. K. W. Kenway, and J. R. R. A. Martins

    Journal of Aircraft, 57(6):1014–1025, 2020

    doi:10.2514/1.C035845

    Details
  6. Tilt-wing eVTOL takeoff trajectory optimization

    S. S. Chauhan, and J. R. R. A. Martins

    Journal of Aircraft, 57(1):93–112, 2020

    doi:10.2514/1.C035476

    Details
  7. DAFoam: An Open-Source Adjoint Framework for Multidisciplinary Design Optimization with OpenFOAM

    P. He, C. A. Mader, J. R. R. A. Martins, and K. J. Maki

    AIAA Journal, 58(3), 2020

    doi:10.2514/1.J058853

    Details
  8. Flexible Formulation of Spatial Integration Constraints in Aerodynamic Shape Optimization

    B. J. Brelje, J. Anibal, A. Yildirim, C. A. Mader, and J. R. R. A. Martins

    AIAA Journal, 58(6):2571–2580, 2020

    doi:10.2514/1.J058366

    Details
  9. Natural Laminar-Flow Airfoil Optimization Design Using a Discrete Adjoint Approach

    Y. Shi, C. A. Mader, S. He, G. L. O. Halila, and J. R. R. A. Martins

    AIAA Journal, 58(11):4702–4722, 2020

    doi:10.2514/1.J058944

    Details
  10. Mixed-integer Second-order Cone Optimization for Composite Discrete Ply-angle and Thickness Topology Optimization Problems

    S. He, M. Shahabsafa, W. Lei, A. Mohammad–Nezhad, T. Terlaky, L. Zuluaga, and J. R. R. A. Martins

    Optimization and Engineering, 2020

    doi:10.1007/s11081-020-09573-0

    Details
  11. Scalable gradient-enhanced artificial neural networks for airfoil shape design in the subsonic and transonic regimes

    M. A. Bouhlel, S. He, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 611363–1376, 2020

    doi:10.1007/s00158-020-02488-5

    Details
  12. Integrated Design Optimization of Spar Floating Wind Turbines

    J. M. Hegseth, E. E. Bachynski, and J. R. R. A. Martins

    Marine Structures, 72102771, 2020

    doi:10.1016/j.marstruc.2020.102771

    Details
  13. Aerostructural Design Exploration of a Wing in Transonic Flow

    N. P. Bons, and J. R. R. A. Martins

    Aerospace, 7(8):118, 2020

    doi:10.3390/aerospace7080118

    Details
  14. Large-Scale Path-Dependent Optimization of Supersonic Aircraft

    J. Jasa, B. Brelje, J. Gray, C. A. Mader, and J. R. R. A. Martins

    Aerospace, 7(152), 2020

    doi:10.3390/aerospace7100152

    Details
  15. Design Optimization of Spar Floating Wind Turbines Considering Different Control Strategies

    J. M. Hegseth, E. E. Bachynski, and J. R. R. A. Martins

    Journal of Physics: Conference Series, 1669012010, 2020

    doi:10.1088/1742-6596/1669/1/012010

    Details
  16. pyOptSparse: A Python framework for large-scale constrained nonlinear optimization of sparse systems

    N. Wu, G. Kenway, C. A. Mader, J. Jasa, and J. R. R. A. Martins

    Journal of Open Source Software, 5(54):2564, 2020

    doi:10.21105/joss.02564

    Details
  17. Aerostructural Trade-offs for Tow-steered Composite Wings

    T. R. Brooks, J. R. R. A. Martins, and G. J. Kennedy

    Journal of Aircraft, 57(5):787–799, 2020

    doi:10.2514/1.C035699

    Details
  18. Multidisciplinary design optimization framework with coupled derivative computation for hybrid aircraft

    A. Sgueglia, ro, P. Schmollgruber, N. Bartoli, E. Benard, J. Morlier, J. Jasa, J. R. R. A. Martins, J. T. Hwang, and J. S. Gray

    Journal of Aircraft, 57(4):715–729, 2020

    doi:10.2514/1.C035509

    Details

2019

  1. Truss topology design optimization with guaranteed kinematic stability

    M. Shahabsafa, R. Fakhimi, W. Lei, T. Terlaky, L. Zuluaga, S. He, J. T. Hwang, and J. R. R. A. Martins

    Lehigh University ISE technical report, 2019

    Details
  2. Experimental Investigation of a Hydrofoil Designed via Hydrostructural Optimization

    N. Garg, B. W. Pearce, Br, P. A. ner, A. W. Phillips, J. R. R. A. Martins, and Y. L. Young

    Journal of Fluids and Structures, 84243–262, 2019

    doi:10.1016/j.jfluidstructs.2018.10.010

    Details
  3. RANS-based Aerodynamic Shape Optimization of a Strut-braced Wing with Overset Meshes

    N. R. Secco, and J. R. R. A. Martins

    Journal of Aircraft, 56(1):217–227, 2019

    doi:10.2514/1.C034934

    Details
  4. Sweep and anisotropy effects on the viscous hydroelastic response of composite hydrofoils

    Y. Liao, J. R. R. A. Martins, and Y. L. Young

    Composite Structures, 230111471, 2019

    doi:10.1016/j.compstruct.2019.111471

    Details
  5. Flutter and Post-Flutter Constraints in Aircraft Design Optimization

    E. Jonsson, C. Riso, C. A. Lupp, C. E. S. Cesnik, J. R. R. A. Martins, and B. I. Epureanu

    Progress in Aerospace Sciences, 109100537, 2019

    doi:10.1016/j.paerosci.2019.04.001

    Details
  6. High-fidelity design-allocation optimization of a commercial aircraft maximizing airline profit

    J. T. Hwang, J. Jasa, and J. R. R. A. Martins

    Journal of Aircraft, 56(3):1165–1178, 2019

    doi:10.2514/1.C035082

    Details
  7. Coupled Aeropropulsive Design Optimization of a Boundary-Layer Ingestion Propulsor

    J. S. Gray, and J. R. R. A. Martins

    The Aeronautical Journal, 123(1259):121–137, 2019

    doi:10.1017/aer.2018.120

    Details
  8. Viscous Fluid Structure Interaction Response of Composite Hydrofoils

    Y. Liao, N. Garg, J. R. R. A. Martins, and Y. L. Young

    Composite Structures, 212571–585, 2019

    doi:10.1016/j.compstruct.2019.01.043

    Details
  9. Impact of Morphing Trailing Edge on Mission Performance for the Common Research Model

    D. A. Burdette, and J. R. R. A. Martins

    Journal of Aircraft, 56(1):369–384, 2019

    doi:10.2514/1.C034967

    Details
  10. Monolithic approach towards next generation aircraft design considering airline operations and economics

    S. Roy, W. A. Crossley, K. T. Moore, J. S. Gray, and J. R. R. A. Martins

    Journal of Aircraft, 56(4):1565–1576, 2019

    doi:10.2514/1.C035312

    Details
  11. High-Reynolds Number Transitional Flow Simulation via Parabolized Stability Equations with an Adaptive RANS Solver

    G. L. O. Halila, G. Chen, Y. Shi, K. J. Fidkowski, J. R. R. A. Martins, and M. M. T. de

    Aerospace Science and Technology, 91321–336, 2019

    doi:10.1016/j.ast.2019.05.018

    Details
  12. High-fidelity Aerostructural Optimization of Tow-steered Composite Wings

    T. R. Brooks, J. R. R. A. Martins, and G. J. Kennedy

    Journal of Fluids and Structures, 88122–147, 2019

    doi:10.1016/j.jfluidstructs.2019.04.005

    Details
  13. Data-based Approach for Fast Airfoil Analysis and Optimization

    J. Li, M. A. Bouhlel, and J. R. R. A. Martins

    AIAA Journal, 57(2):581–596, 2019

    doi:10.2514/1.J057129

    Details
  14. Multipoint high-fidelity CFD-based aerodynamic shape optimization of a 10 MW wind turbine

    M. H. A. Madsen, F. Zahle, N. N. Sørensen, and J. R. R. A. Martins

    Wind Energy Science, 4163–192, 2019

    doi:10.5194/wes-4-163-2019

    Details
  15. Robust aerodynamic shape optimization—from a circle to an airfoil

    X. He, J. Li, C. A. Mader, A. Yildirim, and J. R. R. A. Martins

    Aerospace Science and Technology, 8748–61, 2019

    doi:10.1016/j.ast.2019.01.051

    Details
  16. Design Optimization for Self-Propulsion of a Bulk Carrier Hull Using a Discrete Adjoint Method

    P. He, G. Filip, J. R. R. A. Martins, and K. J. Maki

    Computers & Fluids, 192104259, 2019

    doi:10.1016/j.compfluid.2019.104259

    Details
  17. Aerothermal Optimization of a Ribbed U-Bend Cooling Channel Using the Adjoint Method

    P. He, J. R. R. A. Martins, C. A. Mader, and K. Maki

    International Journal of Heat and Mass Transfer, 140152–172, 2019

    doi:10.1016/j.ijheatmasstransfer.2019.05.075

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  18. Data-driven Constraint Approach to Ensure Low-speed Performance in Transonic Aerodynamic Shape Optimization

    J. Li, S. He, and J. R. R. A. Martins

    Aerospace Science and Technology, 92536–550, 2019

    doi:10.1016/j.ast.2019.06.008

    Details
  19. Electric, Hybrid, and Turboelectric Fixed-Wing Aircraft: A Review of Concepts, Models, and Design Approaches

    B. Brelje, and J. R. R. A. Martins

    Progress in Aerospace Sciences, 1041–19, 2019

    doi:10.1016/j.paerosci.2018.06.004

    Details
  20. A Python surrogate modeling framework with derivatives

    M. A. Bouhlel, J. T. Hwang, N. Bartoli, R. Lafage, J. Morlier, and J. R. R. A. Martins

    Advances in Engineering Software, 135102662, 2019

    doi:10.1016/j.advengsoft.2019.03.005

    Details
  21. Gradient-enhanced kriging for high-dimensional problems

    M. A. Bouhlel, and J. R. R. A. Martins

    Engineering with Computers, 1(35):157–173, 2019

    doi:10.1007/s00366-018-0590-x

    Details
  22. Multimodality in Aerodynamic Wing Design Optimization

    N. P. Bons, X. He, C. A. Mader, and J. R. R. A. Martins

    AIAA Journal, 57(3):1004–1018, 2019

    doi:10.2514/1.J057294

    Details
  23. Adaptive modeling strategy for constrained global optimization with application to aerodynamic wing design

    N. Bartoli, T. Lefebvre, S. Dubreuil, R. Olivanti, R. Priem, N. Bons, J. R. R. A. Martins, and J. Morlier

    Aerospace Science and Technology, 9085–102, 2019

    doi:10.1016/j.ast.2019.03.041

    Details
  24. A Jacobian-free approximate Newton–Krylov startup strategy for RANS simulations

    A. Yildirim, G. K. W. Kenway, C. A. Mader, and J. R. R. A. Martins

    Journal of Computational Physics, 397108741, 2019

    doi:10.1016/j.jcp.2019.06.018

    Details
  25. Effective Adjoint Approaches for Computational Fluid Dynamics

    G. K. W. Kenway, C. A. Mader, P. He, and J. R. R. A. Martins

    Progress in Aerospace Sciences, 110100542, 2019

    doi:10.1016/j.paerosci.2019.05.002

    Details
  26. OpenMDAO: An open-source framework for multidisciplinary design, analysis, and optimization

    J. S. Gray, J. T. Hwang, J. R. R. A. Martins, K. T. Moore, and B. A. Naylor

    Structural and Multidisciplinary Optimization, 59(4):1075–1104, 2019

    doi:10.1007/s00158-019-02211-z

    Details

2018

  1. A fast-prediction surrogate model for large datasets

    J. T. Hwang, and J. R. R. A. Martins

    Aerospace Science and Technology, 7574–87, 2018

    doi:10.1016/j.ast.2017.12.030

    Details
  2. A computational architecture for coupling heterogeneous numerical models and computing coupled derivatives

    J. T. Hwang, and J. R. R. A. Martins

    ACM Transactions on Mathematical Software, 44(4):Article 37, 2018

    doi:10.1145/3182393

    Details
  3. An Aerodynamic Design Optimization Framework Using a Discrete Adjoint Approach with OpenFOAM

    P. He, C. A. Mader, J. R. R. A. Martins, and K. J. Maki

    Computers & Fluids, 168285–303, 2018

    doi:10.1016/j.compfluid.2018.04.012

    Details
  4. Component-based Geometry Manipulation for Aerodynamic Shape Optimization with Overset Meshes

    N. R. Secco, J. P. Jasa, G. K. W. Kenway, and J. R. R. A. Martins

    AIAA Journal, 56(9):3667–3679, 2018

    doi:10.2514/1.J056550

    Details
  5. Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings

    T. R. Brooks, G. K. W. Kenway, and J. R. R. A. Martins

    AIAA Journal, 56(7):2840–2855, 2018

    doi:10.2514/1.J056603

    Details
  6. Modeling Boundary Layer Ingestion Using a Coupled Aeropropulsive Analysis

    J. S. Gray, C. A. Mader, G. K. W. Kenway, and J. R. R. A. Martins

    Journal of Aircraft, 55(3):1191–1199, 2018

    doi:10.2514/1.C034601

    Details
  7. On Manufacturing Constraints for Tow-steered Composite Design Optimization

    T. R. Brooks, and J. R. R. A. Martins

    Composite Structures, 204548–559, 2018

    doi:10.1016/j.compstruct.2018.07.100

    Details
  8. Open-source coupled aerostructural optimization using Python

    J. P. Jasa, J. T. Hwang, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 57(4):1815–1827, 2018

    doi:10.1007/s00158-018-1912-8

    Details
  9. An automated selection algorithm for nonlinear solvers in MDO

    S. S. Chauhan, J. T. Hwang, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 58(2):349–377, 2018

    doi:10.1007/s00158-018-2004-5

    Details
  10. A novel approach to discrete truss design problems using mixed integer neighborhood search

    M. Shahabsafa, A. Mohammad–Nezhad, T. Terlaky, L. Zuluaga, S. He, J. T. Hwang, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 582411—2429, 2018

    doi:10.1007/s00158-018-2099-8

    Details
  11. Design of a Transonic Wing with an Adaptive Morphing Trailing Edge via Aerostructural Optimization

    D. A. Burdette, and J. R. R. A. Martins

    Aerospace Science and Technology, 81192–203, 2018

    doi:10.1016/j.ast.2018.08.004

    Details
  12. On the Influence of Optimization Algorithm and Starting Design on Wing Aerodynamic Shape Optimization

    Y. Yu, Z. Lyu, Z. Xu, and J. R. R. A. Martins

    Aerospace Science and Technology, 75183–199, 2018

    doi:10.1016/j.ast.2018.01.016

    Details

2017

  1. Aerodynamic Shape Optimization of Wind Turbine Blades Using a Reynolds-Averaged Navier–Stokes Model and an Adjoint Method

    T. Dhert, T. Ashuri, and J. R. R. A. Martins

    Wind Energy, 20(5):909–926, 2017

    doi:10.1002/we.2070

    Details
  2. Buffet-Onset Constraint Formulation for Aerodynamic Shape Optimization

    G. K. W. Kenway, and J. R. R. A. Martins

    AIAA Journal, 55(6):1930–1947, 2017

    doi:10.2514/1.J055172

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  3. Expected Drag Minimization for Aerodynamic Design Optimization Based on Aircraft Operational Data

    R. P. Liem, J. R. R. A. Martins, and G. K. Kenway

    Aerospace Science and Technology, 63344–362, 2017

    doi:10.1016/j.ast.2017.01.006

    Details
  4. An Evaluation of Constraint Aggregation Strategies for Wing Box Mass Minimization

    A. B. Lambe, J. R. R. A. Martins, and G. J. Kennedy

    Structural and Multidisciplinary Optimization, 55(1):257–277, 2017

    doi:10.1007/s00158-016-1495-1

    Details
  5. High-fidelity Multipoint Hydrostructural Optimization of a 3-D Hydrofoil

    N. Garg, G. K. W. Kenway, J. R. R. A. Martins, and Y. L. Young

    Journal of Fluids and Structures, 7115–39, 2017

    doi:10.1016/j.jfluidstructs.2017.02.001

    Details
  6. Chemical Equilibrium Analysis with Adjoint Derivatives for Propulsion Cycle Analysis

    J. S. Gray, J. Chin, T. Hearn, E. Hendricks, T. Lavelle, and J. R. R. A. Martins

    Journal of Propulsion and Power, 33(5):1041–1052, 2017

    doi:10.2514/1.B36215

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2016

  1. A Matrix-Free Augmented Lagrangian Algorithm with Application to Large-Scale Structural Design Optimization

    S. Arreckx, A. B. Lambe, J. R. R. A. Martins, and D. Orban

    Optimization and Engineering, 17(2):359–384, 2016

    doi:10.1007/s11081-015-9287-9

    Details
  2. Aeroservoelastic Design Definition of a 20 MW Common Research Wind Turbine Model

    T. Ashuri, J. R. R. A. Martins, M. B. Zaaijer, K. G. A. van, and B. G. J. van

    Wind Energy, 19(11):2071—2087, 2016

    doi:10.1002/we.1970

    Details
  3. Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing

    G. K. W. Kenway, and J. R. R. A. Martins

    AIAA Journal, 54(1):113–128, 2016

    doi:10.2514/1.J054154

    Details
  4. Multidisciplinary Design Optimization of Large Wind Turbines—Technical, Economic, and Design Challenges

    T. Ashuri, M. B. Zaaijer, J. R. R. A. Martins, and J. Zhang

    Energy Conversion and Management, 12356–70, 2016

    doi:10.1016/j.enconman.2016.06.004

    Details
  5. Aerodynamic Shape Optimization of the Common Research Model Wing-Body-Tail Configuration

    S. Chen, Z. Lyu, G. K. W. Kenway, and J. R. R. A. Martins

    Journal of Aircraft, 53(1):276–293, 2016

    doi:10.2514/1.C033328

    Details
  6. An unstructured quadrilateral mesh generation algorithm for aircraft structures

    J. T. Hwang, and J. R. R. A. Martins

    Aerospace Science and Technology, 59172–182, 2016

    doi:10.1016/j.ast.2016.10.010

    Details
  7. Matrix-free aerostructural optimization of aircraft wings

    A. B. Lambe, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 53(3):589–603, 2016

    doi:10.1007/s00158-015-1349-2

    Details

2015

  1. High-fidelity Hydrodynamic Shape Optimization of a 3-D Hydrofoil

    N. Garg, G. K. W. Kenway, Z. Lyu, J. R. R. A. Martins, and Y. L. Young

    Journal of Ship Research, 59(4):209–226, 2015

    doi:10.5957/JOSR.59.4.150046

    Details
  2. Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark

    Z. Lyu, G. K. W. Kenway, and J. R. R. A. Martins

    AIAA Journal, 53(4):968–985, 2015

    doi:10.2514/1.J053318

    Details
  3. Aerodynamic Shape Optimization of an Adaptive Morphing Trailing Edge Wing

    Z. Lyu, and J. R. R. A. Martins

    Journal of Aircraft, 52(6):1951–1970, 2015

    doi:10.2514/1.C033116

    Details
  4. Multimission Aircraft Fuel Burn Minimization via Multipoint Aerostructural Optimization

    R. P. Liem, G. K. W. Kenway, and J. R. R. A. Martins

    AIAA Journal, 53(1):104–122, 2015

    doi:10.2514/1.J052940

    Details
  5. Surrogate Models and Mixtures of Experts in Aerodynamic Performance Prediction for Aircraft Mission Analysis

    R. P. Liem, C. A. Mader, and J. R. R. A. Martins

    Aerospace Science and Technology, 43126–151, 2015

    doi:10.1016/j.ast.2015.02.019

    Details

2014

  1. Scalable Parallel Approach for High-Fidelity Steady-State Aeroelastic Analysis and Adjoint Derivative Computations

    G. K. W. Kenway, G. J. Kennedy, and J. R. R. A. Martins

    AIAA Journal, 52(5):935–951, 2014

    doi:10.2514/1.J052255

    Details
  2. Multidisciplinary Design Optimization of Offshore Wind Turbines for Minimum Levelized Cost of Energy

    T. Ashuri, M. B. Zaaijer, J. R. R. A. Martins, B. G. J. W. van, and K. G. A. M. van

    Renewable Energy, 68893–905, 2014

    doi:10.1016/j.renene.2014.02.045

    Details
  3. Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration

    G. K. W. Kenway, and J. R. R. A. Martins

    Journal of Aircraft, 51(1):144–160, 2014

    doi:10.2514/1.C032150

    Details
  4. Concurrent Aerostructural Topology Optimization of a Wing Box

    K. A. James, G. J. Kennedy, and J. R. R. A. Martins

    Computers and Structures, 1341–17, 2014

    doi:10.1016/j.compstruc.2013.12.007

    Details
  5. Design of a lithium-ion battery pack for PHEV using a hybrid optimization method

    N. Xue, W. Du, T. A. Greszler, W. Shyy, and J. R. R. A. Martins

    Applied Energy, 115591–602, 2014

    doi:10.1016/j.apenergy.2013.10.044

    Details
  6. A Parallel Finite-Element Framework for Large-Scale Gradient-Based Design Optimization of High-Performance Structures

    G. J. Kennedy, and J. R. R. A. Martins

    Finite Elements in Analysis and Design, 8756–73, 2014

    doi:10.1016/j.finel.2014.04.011

    Details
  7. A Surrogate-Based Multi-Scale Model for Mass Transport and Electrochemical Kinetics in Lithium-Ion Battery Electrodes

    W. Du, N. Xue, W. Shyy, and J. R. R. A. Martins

    Journal of the Electrochemical Society, 161(8):E3086–E3096, 2014

    doi:10.1149/2.013408jes

    Details
  8. Aerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft

    Z. Lyu, and J. R. R. A. Martins

    Journal of Aircraft, 51(5):1604–1617, 2014

    doi:10.2514/1.C032491

    Details
  9. Optimization of the Kinematics of a Flapping Wing MAV in Hover for Enhanced Performance

    A. Gogulapati, P. P. Friedmann, and J. R. R. A. Martins

    AIAA Journal, 52(10):2342–2354, 2014

    doi:10.2514/1.J053083

    Details
  10. Large-Scale Multidisciplinary Optimization of a Small Satellite’s Design and Operation

    J. T. Hwang, D. Y. Lee, J. W. Cutler, and J. R. R. A. Martins

    Journal of Spacecraft and Rockets, 51(5):1648–1663, 2014

    doi:10.2514/1.A32751

    Details
  11. Portugueses em IO pelo Mundo—Joaquim R. R. A. Martins

    J. R. R. A. Martins

    Boletim APDIO, (50):15, 2014

    Details
  12. Computing Stability Derivatives and their Gradients for Aerodynamic Shape Optimization

    C. A. Mader, and J. R. R. A. Martins

    AIAA Journal, 52(11):2533–2546, 2014

    doi:10.2514/1.J052922

    Details
  13. A parallel aerostructural optimization framework for aircraft design studies

    G. J. Kennedy, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 50(6):1079–1101, 2014

    doi:10.1007/s00158-014-1108-9

    Details
  14. Wing Design via Numerical Optimization

    J. R. R. A. Martins

    SIAG/OPT Views-and-News, 23(2):2–6, 2014

    Details

2013

  1. Stability-Constrained Aerodynamic Shape Optimization of Flying Wings

    C. A. Mader, and J. R. R. A. Martins

    Journal of Aircraft, 50(5):1431–1449, 2013

    doi:10.2514/1.C031956

    Details
  2. Optimization of a Single Lithium-ion Battery Cell with a Gradient-based Algorithm

    N. Xue, W. Du, A. Gupta, W. Shyy, A. M. Sastry, and J. R. R. A. Martins

    Journal of the Electrochemical Society, 160(8):A1071–A1078, 2013

    doi:10.1149/2.036308jes

    Details
  3. A Laminate Parametrization Technique for Discrete Ply-Angle Problems with Manufacturing Constraints

    G. J. Kennedy, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 48(2):379–393, 2013

    doi:10.1007/s00158-013-0906-9

    Details
  4. Optimization of LiMn2O4 Electrode Properties in a Gradient- and Surrogate-Based Framework

    W. Du, N. Xue, A. Gupta, A. M. Sastry, J. R. R. A. Martins, and W. Shyy

    Acta Mechanica Sinica, 29(3):335–347, 2013

    doi:10.1007_s10409-013-0039-x

    Details
  5. Energy Density Comparison of Li-ion Cathode Materials using Dimensional Analysis

    W. Du, N. Xue, A. M. Sastry, J. R. R. A. Martins, and W. Shyy

    Journal of The Electrochemical Society, 160(8):A1187–A1193, 2013

    doi:10.1149/2.069308jes

    Details
  6. Simultaneous Optimization of Propeller-Hull Systems to Minimize Lifetime Fuel Consumption

    M. Nelson, D. Temple, J. T. Hwang, Y. L. Young, J. R. R. A. Martins, and M. Collette

    Applied Ocean Research, 4346–52, 2013

    doi:10.1016/j.apor.2013.07.004

    Details
  7. Review and Unification of Methods for Computing Derivatives of Multidisciplinary Computational Models

    J. R. R. A. Martins, and J. T. Hwang

    AIAA Journal, 51(11):2582–2599, 2013

    doi:10.2514/1.J052184

    Details
  8. Multidisciplinary Design Optimization: A Survey of Architectures

    J. R. R. A. Martins, and A. B. Lambe

    AIAA Journal, 51(9):2049–2075, 2013

    doi:10.2514/1.J051895

    Details

2012

  1. Model-Predictive Gust Load Alleviation Controller for a Highly Flexible Aircraft

    S. Haghighat, H. H. T. Liu, and J. R. R. A. Martins

    Journal of Guidance, Control and Dynamics, 35(6):1751–1766, 2012

    doi:10.2514/1.57013

    Details
  2. A homogenization-based theory for anisotropic beams with accurate though-section stress and strain prediction

    G. J. Kennedy, and J. R. R. A. Martins

    International Journal of Solids and Structures, 49(1):54–72, 2012

    doi:10.1016/j.ijsolstr.2011.09.012

    Details
  3. Stress-Based Topology Optimization Using an Isoparametric Level Set Method

    K. A. James, E. Lee, and J. R. R. A. Martins

    Finite Elements in Analysis and Design, 5820–30, 2012

    doi:10.1016/j.finel.2012.03.012

    Details
  4. Derivatives for Time-Spectral Computational Fluid Dynamics Using an Automatic Differentiation Adjoint

    C. A. Mader, and J. R. R. A. Martins

    AIAA Journal, 50(12):2809–2819, 2012

    doi:10.2514/1.J051658

    Details
  5. Extensions to the Design Structure Matrix for the Description of Multidisciplinary Design, Analysis, and Optimization Processes

    A. B. Lambe, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 46273–284, 2012

    doi:10.1007/s00158-012-0763-y

    Details
  6. Aerostructural optimization of a composite wing

    G. J. Kennedy, and J. R. R. A. Martins

    2012

    Details
  7. Stress-Constrained Topology Optimization with Design-Dependent Loading

    E. Lee, K. A. James, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 46647–661, 2012

    doi:10.1007/s00158-012-0780-x

    Details
  8. Aircraft Conceptual Design for Optimal Environmental Performance

    R. P. Henderson, J. R. R. A. Martins, and R. E. Perez

    The Aeronautical Journal, 116(1175):1–22, 2012

    Details
  9. Aeroservoelastic Design Optimization of a Flexible Wing

    S. Haghighat, J. R. R. A. Martins, and H. H. T. Liu

    Journal of Aircraft, 49(2):432–443, 2012

    doi:10.2514/1.C031344

    Details
  10. pyOpt: A Python-Based Object-Oriented Framework for Nonlinear Constrained Optimization

    R. E. Perez, P. W. Jansen, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 45(1):101–118, 2012

    doi:10.1007/s00158-011-0666-3

    Details
  11. Structural Topology Optimization with Design-Dependent Pressure Loads

    E. Lee, and J. R. R. A. Martins

    Computer Methods in Applied Mechanics and Engineering, 233–23640–48, 2012

    doi:10.1016/j.cma.2012.04.007

    Details
  12. An Isoparametric Approach to Level Set Topology Optimization Using a Body-Fitted Finite Element Mesh

    K. A. James, and J. R. R. A. Martins

    Computers and Structures, 90–9197–106, 2012

    doi:10.1016/j.compstruc.2011.10.004

    Details

2011

  1. Adaptive Accuracy Trust Region: Using Cross-Validation in the Optimization Process

    Q. Thomson, and J. R. R. A. Martins

    Engineering Optimization, 43(6):615–633, 2011

    doi:10.1080/0305215X.2010.508521

    Details
  2. Multidisciplinary Design Optimization for Complex Engineered Systems Design: Report from an NSF Workshop

    T. W. Simpson, and J. R. R. A. Martins

    Journal of Mechanical Design, 133(10):101002, 2011

    doi:10.1115/1.4004465

    Details
  3. Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach

    C. A. Mader, and J. R. R. A. Martins

    AIAA Journal, 49(12):2737–2750, 2011

    doi:10.2514/1.J051147

    Details
  4. A Timoshenko beam theory with pressure corrections for layered orthotropic beams

    G. J. Kennedy, J. S. Hansen, and J. R. R. A. Martins

    International Journal of Solids and Structures, 48(16-17):2373–2382, 2011

    doi:10.1016/j.ijsolstr.2011.04.009

    Details
  5. Aerostructural design optimization of composite aircraft with stress and local buckling constraints using an implicit structural parametrization

    G. J. Kennedy, and J. R. R. A. Martins

    Proceedings of CASI AERO 2011, 2011

    Details

2010

  1. Aerostructural Optimization of Nonplanar Lifting Surfaces

    P. Jansen, R. E. Perez, and J. R. R. A. Martins

    Journal of Aircraft, 47(5):1491–1503, 2010

    doi:10.2514/1.44727

    Details
  2. Benchmarking Multidisciplinary Design Optimization Algorithms

    N. P. Tedford, and J. R. R. A. Martins

    Optimization and Engineering, 11(1):159–183, 2010

    doi:10.1007/s11081-009-9082-6

    Details
  3. Editorial—Special Issue on Optimization and Engineering Applications

    J. R. R. A. Martins, and E. A. Kostina

    Optimization and Engineering, 11(1):1–3, 2010

    doi:10.1007/s11081-010-9105-3

    Details

2009

  1. Structural Topology Optimization for Multiple Load Cases Using a Dynamic Aggregation Technique

    K. James, J. S. Hansen, and J. R. R. A. Martins

    Engineering Optimization, 41(12):1103–1118, 2009

    doi:10.1080/03052150902926827

    Details
  2. pyMDO: An Object-Oriented Framework for Multidisciplinary Design Optimization

    J. R. R. A. Martins, C. Marriage, and N. P. Tedford

    ACM Transactions on Mathematical Software, 36(4):20:1–20:25, 2009

    doi:10.1145/1555386.1555389

    Details
  3. An Asymmetric Suboptimization Approach to Aerostructural Optimization

    I. R. Chittick, and J. R. R. A. Martins

    Optimization and Engineering, 10(1):133–152, 2009

    doi:10.1007/s11081-008-9046-2

    Details

2008

  1. ADjoint: An Approach for the Rapid Development of Discrete Adjoint Solvers

    C. A. Mader, J. R. R. A. Martins, J. J. Alonso, and d. W. E. van

    AIAA Journal, 46(4):863-873, 2008

    doi:10.2514/1.29123

    Details
  2. Aero-Structural Optimization Using Adjoint Coupled Post-Optimality Sensitivities

    I. R. Chittick, and J. R. R. A. Martins

    Structures and Multidisciplinary Optimization, 3659–70, 2008

    doi:10.1007/s00158-007-0200-9

    Details

2007

  1. An Adaptive Approach to Constraint Aggregation Using Adjoint Sensitivity Analysis

    N. M. K. Poon, and J. R. R. A. Martins

    Structural and Multidisciplinary Optimization, 34(1):61–73, 2007

    doi:10.1007/s00158-006-0061-7

    Details
  2. A methodology for the development of discrete adjoint solvers using automatic differentiation tools

    A. C. Marta, C. A. Mader, J. R. R. A. Martins, d. W. E. van, and J. J. Alonso

    International Journal of Computational Fluid Dynamics, 21(9):307-327, 2007

    doi:10.1080/10618560701678647

    Details

2006

  1. Variable-complexity optimization applied to airfoil design

    P. Thokala, and J. R. R. A. Martins

    Engineering Optimization, 39(3):271–286, 2006

    doi:10.1080/03052150601107976

    Details

2005

  1. A Coupled-Adjoint Sensitivity Analysis Method for High-Fidelity Aero-Structural Design

    J. R. R. A. Martins, J. J. Alonso, and J. J. Reuther

    Optimization and Engineering, 6(1):33–62, 2005

    doi:10.1023/B:OPTE.0000048536.47956.62

    Details

2004

  1. High-Fidelity Aerostructural Design Optimization of a Supersonic Business Jet

    J. R. R. A. Martins, J. J. Alonso, and J. J. Reuther

    Journal of Aircraft, 41(3):523–530, 2004

    doi:10.2514/1.11478

    Details

2003

  1. The Complex-Step Derivative Approximation

    J. R. R. A. Martins, P. Sturdza, and J. J. Alonso

    ACM Transactions on Mathematical Software, 29(3):245–262, 2003

    doi:10.1145/838250.838251

    Details

2021

  1. Geometrically Nonlinear High-fidelity Aerostructural Optimization for Highly Flexible Wings

    A. C. Gray, and J. R. R. A. Martins

    Proceedings of the AIAA SciTech Forum, 2021

    doi:10.2514/6.2021-0283

    Details
  2. Coupled Aeropropulsive Design Optimization of a Podded Electric Propulsor

    A. Yildirim, J. S. Gray, C. A. Mader, and J. R. R. A. Martins

    AIAA Aviation Forum, 2021

    doi:10.2514/6.2021-3032

    Details
  3. Performance Analysis of Optimized STARC-ABL Designs Across the Entire Mission Profile

    A. Yildirim, J. S. Gray, C. A. Mader, and J. R. R. A. Martins

    Proceedings of the AIAA SciTech Forum, 2021

    doi:10.2514/6.2021-0891

    Details
  4. A hybrid time-spectral approach for aerodynamic shape optimization with unsteady flow

    P. He, , and R. R. A. M. Joaquim

    Proceedings of the AIAA SciTech Forum, 2021

    doi:10.2514/6.2021-0278

    Details
  5. An efficient nonlinear reduced-order modeling approach for rapid aerodynamic analysis with OpenFOAM

    P. He, R. Halder, K. J. Fidkowski, K. J. Maki, and J. R. R. A. Martins

    Proceedings of the AIAA SciTech Forum, 2021

    doi:10.2514/6.2021-1476

    Details
  6. Aerostructural Wing Optimization for a Hydrogen Fuel Cell Aircraft

    B. J. Brelje, and J. R. R. A. Martins

    Proceedings of the AIAA SciTech Forum, 2021

    doi:10.2514/6.2021-1132

    Details
  7. Predicting the High Angle of Attack Characteristics of a Delta Wing at Low Speed

    S. Seraj, and J. R. R. A. Martins

    AIAA Aviation Forum, 2021

    doi:10.2514/6.2021-2612

    Details

2020

  1. High-fidelity Aerostructural Optimization Studies of the Aerion AS2 Supersonic Business Jet

    N. P. Bons, J. R. R. A. Martins, C. A. Mader, M. McMullen, and M. Suen

    Proceedings of the AIAA Aviation Forum, 2020

    doi:10.2514/6.2020-3182

    Details
  2. Aerostructural Wing Design Exploration with Multidisciplinary Design Optimization

    N. P. Bons, and J. R. R. A. Martins

    Proceedings of the AIAA SciTech Forum, 2020

    doi:10.2514/6.2020-0544

    Details
  3. A B-Spline-based Generative Adversarial Network Model for Fast Interactive Airfoil Aerodynamic Optimization

    X. Du, P. He, and J. R. R. A. Martins

    AIAA SciTech Forum, 2020

    doi:10.2514/6.2020-2128

    Details
  4. Aerothermal Optimization of X-57 High-Lift Motor Nacelle

    J. L. Anibal, C. A. Mader, and J. R. R. A. Martins

    AIAA SciTech Forum, 2020

    doi:10.2514/6.2020-2115

    Details
  5. A Time-Spectral Adjoint Approach for Aerodynamic Shape Optimization Under Periodic Wakes

    P. He, A. J. Luder, C. A. Mader, K. J. Maki, and J. R. R. A. Martins

    AIAA SciTech Forum, 2020

    doi:10.2514/6.2020-2114

    Details
  6. RANS-Based Aerodynamic Shape Optimization of a Wing Considering Propeller-Wing Interaction

    S. S. Chauhan, and J. R. R. A. Martins

    AIAA SciTech Forum, 2020

    doi:10.2514/6.2020-1764

    Details
  7. Hydrodynamic Optimization of a T-foil

    Y. Liao, A. Yildirim, Y. L. Young, and J. R. R. A. Martins

    SNAME Maritime Convention, 2020

    Details
  8. Hydrostructural Optimization of Generic Composite Hydrofoils

    Y. Liao, S. He, J. R. R. A. Martins, and Y. L. Young

    AIAA SciTech Forum, 2020

    doi:10.2514/6.2020-0164

    Details
  9. Perspectives on Aerodynamic Design Optimization

    J. R. R. A. Martins

    AIAA SciTech Forum, 2020

    doi:10.2514/6.2020-0043

    Details

2019

  1. Multipoint Aerodynamic Shape Optimization for Subsonic and Supersonic Regimes

    M. Mangano, and J. R. R. A. Martins

    57th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, 2019, 2019

    doi:10.2514/6.2019-0696

    Details
  2. Enabling Large-scale Multidisciplinary Design Optimization through Adjoint Sensitivity Analysis

    J. R. R. A. Martins, and G. J. Kennedy

    57th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, 2019

    doi:10.2514/6.2019-1702

    Details
  3. CFD-based Aircraft Design Optimization

    J. R. R. A. Martins

    Proceedings of the International Conference on Flow Dynamics, 2019

    Details
  4. How Certain Physical Considerations Impact Aerostructural Wing Optimization

    J. P. Jasa, S. S. Chauhan, J. S. Gray, and J. R. R. A. Martins

    AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2019

    doi:10.2514/6.2019-3242

    Details
  5. Multi-fidelity efficient global optimization: Methodology and application to airfoil shape design

    N. Bartoli, M. Meliani, J. Morlier, T. Lefebvre, M. Bouhlel, and J. R. R. A. Martins

    AIAA Aviation Forum, 2019

    doi:10.2514/6.2019-3236

    Details
  6. Aeropropulsive Design Optimization of a Boundary Layer Ingestion System

    A. Yildirim, J. S. Gray, C. A. Mader, and J. R. R. A. Martins

    AIAA Aviation Forum, 2019

    doi:10.2514/6.2019-3455

    Details
  7. Development of a Conceptual-Level Thermal Management System Design Capability in OpenConcept

    B. J. Brelje, J. P. Jasa, J. R. R. A. Martins, and J. S. Gray

    NATO Research Symposium on Hybrid/Electric Aero-Propulsion Systems for Military Applications (AVT-RSY-323), 2019

    doi:10.14339/STO-MP-AVT-323

    Details
  8. Coupled component sizing and aerodynamic shape optimization via geometric constraints

    B. J. Brelje, and J. R. R. A. Martins

    AIAA AVIATION Forum, 2019

    doi:10.2514/6.2019-3105

    Details
  9. Flexible Formulation of Spatial Integration Constraints in Aerodynamic Shape Optimization

    B. J. Brelje, J. L. Anibal, A. Yildirim, C. A. Mader, and J. R. R. A. Martins

    57th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, 2019

    doi:10.2514/6.2019-2355

    Details
  10. A Coupled Newton–Krylov Time-Spectral Solver for Wing Flutter and LCO Prediction

    S. He, E. Jonsson, C. A. Mader, and J. R. R. A. Martins

    AIAA Aviation Forum, 2019

    doi:10.2514/6.2019-3549

    Details
  11. Aerodynamic Shape Optimization with Time Spectral Flutter Adjoint

    S. He, E. Jonsson, C. A. Mader, and J. R. R. A. Martins

    2019 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2019

    doi:10.2514/6.2019-0697

    Details
  12. An object-oriented framework for rapid discrete adjoint development using OpenFOAM

    P. He, C. A. Mader, J. R. R. A. Martins, and K. J. Maki

    AIAA Science and Technology Forum and Exposition, 2019

    doi:10.2514/6.2019-1210

    Details
  13. Multipoint Variable Cycle Engine Design Using Gradient-based Optimization

    J. P. Jasa, J. S. Gray, J. A. Seidel, C. A. Mader, and J. R. R. A. Martins

    57th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, 2019, 2019

    doi:10.2514/6.2019-0172

    Details
  14. High-Reynolds Number Transitional Flow Prediction using a Coupled Discontinuous-Galerkin RANS PSE Framework

    G. L. O. Halila, G. Chen, Y. Shi, K. J. Fidkowski, J. R. R. A. Martins, and M. T. Mendonça

    Proceedings of the 57th AIAA Aerospace Sciences Meeting, 2019

    doi:10.2514/6.2019-0974

    Details
  15. Coupled Design of a Supersonic Engine and Thermal System

    J. P. Jasa, B. J. Brelje, C. A. Mader, and J. R. R. A. Martins

    World Congress of Structural and Multidisciplinary Optimization, 2019

    Details
  16. Computational Modeling of Flutter Constraint for High-Fidelity Aerostructural Optimization

    E. Jonsson, C. A. Mader, G. J. Kennedy, and J. R. R. A. Martins

    2019 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2019

    doi:10.2514/6.2019-2354

    Details

2018

  1. Aerothermal optimization of internal cooling passages using a discrete adjoint method

    P. He, C. A. Mader, J. R. R. A. Martins, and K. J. Maki

    AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2018

    doi:10.2514/6.2018-4080

    Details
  2. High-Fidelity Aerodynamic Shape Optimization of a Full Configuration Regional Jet

    N. P. Bons, C. A. Mader, J. R. R. A. Martins, A. P. C. Cuco, and F. I. K. Odaguil

    2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018

    doi:10.2514/6.2018-0106

    Details
  3. Next generation aircraft design considering airline operations and economics

    S. Roy, W. A. Crossley, K. T. Moore, J. S. Gray, and J. R. R. A. Martins

    AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018

    doi:10.2514/6.2018-1647

    Details
  4. Aero-propulsive Design Optimization of a Turboelectric Boundary Layer Ingestion Propulsion System

    J. S. Gray, G. K. W. Kenway, C. A. Mader, and J. R. R. A. Martins

    2018 AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2018

    doi:10.2514/6.2018-3976

    Details
  5. RANS-based Aerodynamic Shape Optimization of a Strut-braced Wing with Overset Meshes

    N. R. Secco, and J. R. R. A. Martins

    2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018

    doi:10.2514/6.2018-0413

    Details
  6. Low-Fidelity Aerostructural Optimization of Aircraft Wings with a Simplified Wingbox Model Using OpenAeroStruct

    S. S. Chauhan, and J. R. R. A. Martins

    Proceedings of the 6th International Conference on Engineering Optimization, EngOpt 2018, 418-431, 2018

    doi:10.1007/978-3-319-97773-7_38

    Details
  7. Transition Prediction Based on Linear Stability Theory with the RANS Solver for Three-Dimensional Configurations

    Y. Shi, R. Gross, C. A. Mader, and J. R. R. A. Martins

    Proceedings of the AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, 2018

    doi:10.2514/6.2018-0819

    Details
  8. Development of a Conceptual Design Model for Aircraft Electric Propulsion with Efficient Gradients

    B. J. Brelje, and J. R. R. A. Martins

    Proceedings of the AIAA/IEEE Electric Aircraft Technologies Symposium, 2018

    doi:10.2514/6.2018-4979

    Details
  9. FlexFoil Shape Adaptive Control Surfaces—Flight Test and Numerical Results

    S. Kota, and J. R. R. A. Martins

    Proceedings of the 31st Congress of the International Council of Aeronautical Sciences, 2018

    Details
  10. Trajectory Optimization of a Supersonic Air Vehicle with Thermal Fuel Management System

    J. P. Jasa, C. A. Mader, and J. R. R. A. Martins

    AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2018

    doi:10.2514/6.2018-3884

    Details
  11. A Coupled Newton–Krylov Time Spectral Solver for Flutter Prediction

    S. He, E. Jonsson, C. A. Mader, and J. R. R. A. Martins

    2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018

    doi:10.2514/6.2018-2149

    Details
  12. Hull form hydrodynamic design using a discrete adjoint optimization method

    P. He, G. Filip, J. R. R. A. Martins, and K. J. Maki

    13th International Marine Design Conference, 2018

    Details
  13. Enabling Modular Aerostructural Optimization: Individual Discipline Feasible without the Jacobians

    A. Dener, J. E. Hicken, G. K. W. Kenway, and J. R. R. A. Martins

    2018 AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2018

    Details

2017

  1. Multimodality in Aerodynamic Wing Design Optimization

    N. P. Bons, X. He, C. A. Mader, and J. R. R. A. Martins

    18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2017

    doi:10.2514/6.2017-3753

    Details
  2. High-fidelity Multipoint Aerostructural Optimization of a High Aspect Ratio Tow-steered Composite Wing

    T. R. Brooks, G. J. Kennedy, and J. R. R. A. Martins

    Proceedings of the 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA SciTech Forum, 2017

    doi:10.2514/6.2017-1350

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  3. Similarity Maximization of a Scaled Aeroelastic Flight Demonstrator via Multidisciplinary Optimization

    J. M. Colomer, N. Bartoli, T. Lefebvre, S. Dubreuil, J. R. R. A. Martins, E. Benard, and J. Morlier

    Proceedings of the AIAA SciTech Conference, 2017

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  4. Aerostructural Optimization of the D8 Wing with Varying Cruise Mach Numbers

    C. A. Mader, G. K. Kenway, J. R. R. A. Martins, A. Uranga, and ra

    18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2017

    doi:10.2514/6.2017-4436

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  5. On the Consequences of the “No Free Lunch” Theorem for Optimization on the Choice of MDO Architecture

    C. Vanaret, F. Gallard, and J. R. R. A. Martins

    Proceedings of the AIAA SciTech Conference, 2017

    Details
  6. Benchmarking approaches for the multidisciplinary analysis of complex systems using a Taylor series-based scalable problem

    S. S. Chauhan, J. T. Hwang, and J. R. R. A. Martins

    12th World Congress on Structural and Multidisciplinary Optimization, 2017

    doi:10.1007/978-3-319-67988-4_7

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  7. An adaptive optimization strategy based on mixture of experts for wing aerodynamic design optimization

    N. Bartoli, T. Lefebvre, S. Dubreuil, R. Olivanti, N. Bons, J. R. R. A. Martins, M. A. Bouhlel, and J. Morlier

    Proceedings of the 18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2017

    doi:10.2514/6.2017-4433

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  8. Component-based Geometry Manipulation for Aerodynamic Shape Optimization with Overset Meshes

    N. R. Secco, J. P. Jasa, G. K. W. Kenway, and J. R. R. A. Martins

    18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2017

    doi:10.2514/6.2017-3327

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  9. Approach to Modeling Boundary Layer Ingestion using a Fully Coupled Propulsion-RANS Model

    J. Gray, C. A. Mader, G. K. W. Kenway, , and R. R. A. M. Joaquim

    55th AIAA Aerospace Sciences Meeting (SciTech), 2017

    doi:10.2514/6.2017-1753

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  10. Undeflected Common Research Model (uCRM): An Aerostructural Model for the Study of High Aspect Ratio Transport Aircraft Wings

    T. R. Brooks, G. K. W. Kenway, and J. R. R. A. Martins

    18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2017

    doi:10.2514/6.2017-4456

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  11. An Efficient Parallel Overset Method for Aerodynamic Shape Optimization

    G. K. W. Kenway, N. Secco, J. R. R. A. Martins, A. Mishra, and K. Duraisamy

    Proceedings of the 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA SciTech Forum, 2017

    doi:10.2514/6.2017-0357

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  12. A Mixed Integer Efficient Global Optimization Algorithm for the Simultaneous Aircraft Allocation-Mission-Design Problem

    S. Roy, K. Moore, J. T. Hwang, J. S. Gray, W. A. Crossley, and J. R. R. A. Martins

    Proceeding of the 58th AIAA Structures, Structural Dynamics, and Materials Conference, 2017

    doi:10.2514/6.2017-1305

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2016

  1. Allocation-mission-design optimization of next-generation aircraft using a parallel computational framework

    J. T. Hwang, and J. R. R. A. Martins

    57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016

    doi:10.2514/6.2016-1662

    Details
  2. Thermodynamics For Gas Turbine Cycles With Analytic Derivatives in OpenMDAO

    J. S. Gray, J. Chin, T. Hearn, E. S. Hendricks, T. M. Lavelle, and J. R. R. A. Martins

    57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016

    doi:10.2514/6.2016-0669

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  3. High-fidelity Coupled Hydrostructural Optimization of a 3-D Hydrofoil

    N. Garg, G. K. W. Kenway, J. R. R. A. Martins, and Y. L. Young

    Proceedings of the International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, 2016

    Details
  4. High-fidelity Aerostructural Optimization of a High Aspect Ratio Tow-steered Wing

    T. R. Brooks, G. J. Kennedy, and J. R. R. A. Martins

    57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016

    doi:10.2514/6.2016-1179

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  5. Aerostructural design optimization of a continuous morphing trailing edge aircraft for improved mission performance

    D. A. Burdette, G. K. W. Kenway, and J. R. R. A. Martins

    17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2016

    doi:10.2514/6.2016-3209

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  6. Performance Evaluation of a Morphing Trailing Edge Using Multipoint Aerostructural Design Optimization

    D. A. Burdette, G. K. Kenway, and J. R. R. A. Martins

    57th AIAA Structures, Structural Dynamics, and Materials Conference, 2016

    doi:10.2514/6.2016-0159

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  7. Aerodynamic Shape Optimization of the CRM Configuration Including Buffet-Onset Conditions

    G. K. Kenway, and J. R. R. A. Martins

    54th AIAA Aerospace Sciences Meeting, 2016

    doi:10.2514/6.2016-1294

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2015

  1. Comparison of Newton–Krylov and Quasi-Newton Algorithms for Aerodynamic Shape Optimization

    A. Dener, J. E. Hicken, G. K. W. Kenway, Z. Lyu, and J. R. R. A. Martins

    Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech), 2015

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  2. Aerodynamic Shape Optimization of the Common Research Model Wing-Body-Tail Configuration

    S. Chen, Z. Lyu, G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech), 2015

    doi:10.2514/6.2015-1718

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  3. High-fidelity aerostructural optimization considering buffet onset

    G. W. K. Kenway, and J. R. R. A. Martins

    Proceedings of the 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015

    doi:10.2514/6.2015-2790

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  4. High-fidelity Hydrodynamic Shape Optimization of a 3-D Morphing Hydrofoil

    N. Garg, Z. Lyu, T. Dhert, J. R. R. A. Martins, and Y. L. Young

    Fourth International Symposium on Marine Propulsors, 2015

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  5. Aerodynamic Shape Optimization of a Truss-Braced-Wing Aircraft

    D. Ivaldi, N. R. Secco, S. Chen, J. T. Hwang, and J. R. R. A. Martins

    Proceedings of the 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015

    doi:10.2514/6.2015-3436

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  6. Parallel allocation-mission optimization of a 128-route network

    J. T. Hwang, and J. R. R. A. Martins

    Proceedings of the 16th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2015

    doi:10.2514/6.2015-2321

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  7. Simultaneous aircraft allocation and mission optimization using a modular adjoint approach

    J. T. Hwang, S. Roy, J. Y. Kao, J. R. R. A. Martins, and W. A. Crossley

    Proceedings of the 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2015

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  8. A Modular Approach for Mission Analysis and Optimization

    J. Y. Kao, J. T. Hwang, and J. R. R. A. Martins

    56th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2015

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  9. A Modular Adjoint Approach to Aircraft Mission Analysis and Optimization

    J. Y. Kao, J. T. Hwang, J. R. R. A. Martins, J. S. Gray, and K. T. Moore

    Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech), 2015

    Details
  10. Shape Optimization with OpenFOAM

    C. A. Mader, J. R. R. A. Martins, and K. J. Maki

    10^th OpenFOAM Workshop, 2015

    Details
  11. Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing

    G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech), 2015

    doi:10.2514/6.2015-0264

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  12. Aerostructural Design Optimization of an Adaptive Morphing Trailing Edge Wing

    D. Burdette, G. K. W. Kenway, Z. Lyu, and J. R. R. A. Martins

    Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech), 2015

    doi:10.2514/6.2016-1294

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2014

  1. Automatic Evaluation of Multidisciplinary Derivatives Using a Graph-Based Problem Formulation in OpenMDAO

    J. S. Gray, T. Hearn, K. Moore, J. T. Hwang, J. R. R. A. Martins, and A. Ning

    Proceedings of the 15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2014

    doi:10.2514/6.2014-2042

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  2. Strategies for Solving High-Fidelity Aerodynamic Shape Optimization Problems

    Z. Lyu, and J. R. R. A. Martins

    15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2014

    doi:10.2514/6.2014-2594

    Details
  3. Geometry and Structural Modeling for High-Fidelity Aircraft Conceptual Design Optimization

    J. T. Hwang, G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the 15th AIAA Multidisciplinary Analysis and Optimization Conference, 2014

    doi:10.2514/6.2014-2041

    Details
  4. RANS-based Aerodynamic Shape Optimization Investigations of the Common Research Model Wing

    Z. Lyu, G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech), 2014

    doi:10.2514/6.2014-0567

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  5. High Aspect Ratio Wing Design: Optimal Aerostructural Tradeoffs for the Next Generation of Materials

    G. J. Kennedy, G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech), 2014

    doi:10.2514/6.2014-0596

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  6. Towards Gradient-Based Design Optimization of Flexible Transport Aircraft with Flutter Constraints

    G. J. Kennedy, G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the 15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2014

    doi:10.2514/6.2014-2726

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  7. Benchmarking Optimization Algorithms for Wing Aerodynamic Design Optimization

    Z. Lyu, Z. Xu, and J. R. R. A. Martins

    Proceedings of the 8th International Conference on Computational Fluid Dynamics, 2014

    Details
  8. Surrogate Models and Mixtures of Experts in Aerodynamic Performance Prediction for Mission Analysis

    R. P. Liem, and J. R. R. A. Martins

    15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2014

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2013

  1. Aerostructural design optimization of a 100-passenger regional jet with surrogate-based mission analysis

    R. P. Liem, C. A. Mader, E. Lee, and J. R. R. A. Martins

    2013 Aviation Technology, Integration, and Operations Conference, 2013

    doi:10.2514/6.2013-4372

    Details
  2. Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft

    Z. Lyu, and J. R. R. A. Martins

    Proceedings of the 51st AIAA Aerospace Sciences Meeting, 2013

    doi:10.2514/6.2013-283

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  3. RANS-based Aerodynamic Shape Optimization of a Blended-Wing-Body Aircraft

    Z. Lyu, and J. R. R. A. Martins

    21st AIAA Computational Fluid Dynamics Conference, 2013

    doi:10.2514/6.2013-2586

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  4. Automatic Differentiation Adjoint of the Reynolds-Averaged Navier–Stokes Equations with a Turbulence Model

    Z. Lyu, G. K. Kenway, C. Paige, and J. R. R. A. Martins

    21st AIAA Computational Fluid Dynamics Conference, 2013

    doi:10.2514/6.2013-2581

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  5. Hybrid-parallel Methods for Large-scale Gradient-based Structural Design Optimization

    G. J. Kennedy, and J. R. Martins

    Proceedings of the 10th World Congress on Structural and Multidisciplinary Optimization, 2013

    Details
  6. Large-Scale MDO of a Small Satellite using a Novel Framework for the Solution of Coupled Systems and their Derivatives

    J. T. Hwang, D. Y. Lee, J. W. Cutler, and J. R. R. A. Martins

    Proceedings of the 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2013

    doi:10.2514/6.2013-1599

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  7. Aeroservoelastic Tailoring of Highly Flexible Transport Wings with Optimal Load Alleviation

    S. Haghighat, J. R. R. A. Martins, and H. H. T. Liu

    Proceedings of the 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2013

    Details
  8. Multifidelity aerostructural optimization of a long-range aircraft configuration with uncertain missions and operating conditions

    R. P. Liem, and J. R. R. A. Martins

    Proceedings of the 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2013

    Details
  9. Optimization of the Kinematics of a Flapping Wing MAV in Hover for Enhanced Performance

    A. Gogulapati, P. P. Friedmann, and J. R. R. A. Martins

    Proceedings of the 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2013

    Details
  10. A Matrix-Free Approach to Large-Scale Structural Optimization

    A. B. Lambe, and J. R. R. A. Martins

    Proceedings of the 10th World Congress on Structural and Multidisciplinary Optimization, 2013

    Details
  11. An Adjoint-based Derivative Evaluation Method for Time-dependent Aeroelastic Optimization of Flexible Aircraft

    G. J. Kennedy, and J. R. R. A. Martins

    Proceedings of the 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2013

    doi:10.2514/6.2013-1530

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2012

  1. Review and Unification of Methods for Computing Derivatives of Multidisciplinary Systems

    J. R. R. A. Martins, and J. T. Hwang

    53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2012

    Details
  2. Multi-point, multi-mission, high-fidelity aerostructural optimization of a long-range aircraft configuration

    R. P. Liem, G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2012

    doi:10.2514/6.2012-5706

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  3. GeoMACH: Geometry-centric MDAO of Aircraft Configurations with High Fidelity

    J. T. Hwang, and J. R. R. A. Martins

    Proceedings of the 14th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, 2012

    doi:10.2514/6.2012-5605

    Details
  4. A Scalable Parallel Approach for High-Fidelity Aerostructural Analysis and Optimization

    G. K. W. Kenway, G. J. Kennedy, and J. R. R. A. Martins

    53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2012

    Details
  5. Optimal Flying Wings: A Numerical Optimization Study

    C. A. Mader, and J. R. R. A. Martins

    53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2012

    Details
  6. Graph Partitioning-Based Coordination Methods for Large-Scale Multidisciplinary Design Optimization Problems

    Z. Lu, and J. R. R. A. Martins

    Proceedings of the 14th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, 2012

    doi:10.2514/6.2012-5522

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  7. Micromechanical Modeling and Design Optimization of 2-D Triaxial Braided Composites

    J. T. Hwang, A. M. Waas, and J. R. R. A. Martins

    Proceedings of the 50th AIAA Aerospace Sciences Meeting, 2012

    Details
  8. A Dynamic Parametrization Scheme for 3-D Shape Optimization Using Quasi-Newton Methods

    J. T. Hwang, and J. R. R. A. Martins

    Proceedings of the 50th AIAA Aerospace Sciences Meeting, 2012

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  9. A Comparison of Metallic and Composite Aircraft Wings Using Aerostructural Design Optimization

    G. J. Kennedy, and J. R. R. A. Martins

    14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2012

    doi:10.2514/6.2012-5475

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  10. A Regularized Discrete Laminate Parametrization Technique with Applications to Wing-Box Design Optimization

    G. J. Kennedy, and J. R. R. A. Martins

    53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2012

    Details

2011

  1. Aeroservoelastic Design Optimization of a High Aspect Ratio Flying Wing

    S. Haghighat, H. H. T. Liu, and J. R. R. A. Martins

    Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, 2011

    Details
  2. A Unified Description of MDO Architectures

    A. B. Lambe, and J. R. R. A. Martins

    Proceedings of the 9th World Congress on Structural and Multidisciplinary Optimization, 2011

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  3. Mixed-Norm Multi-Objective Robust Controller Applied to a Very Flexible Aircraft

    S. Haghighat, H. H. T. Liu, and J. R. R. A. Martins

    Proceedings of the AIAA Guidance, Navigation and Control Conference, 2011

    Details
  4. Aerostructural design optimization of composite aircraft with stress and local buckling constraints using an implicit structural parametrization

    G. J. Kennedy, and J. R. R. A. Martins

    Proceedings of CASI AERO 2011, 2011

    Details
  5. Aerostructural Topology Optimization of an Aircraft Wingbox

    K. A. James, G. J. Kennedy, and J. R. R. A. Martins

    Proceedings of the CASI AERO 2011 Conference, 2011

    Details
  6. Level Set Topology Optimization of Structures with Isoparametric Mesh Mapping

    K. A. James, and J. R. R. A. Martins

    Proceedings of the 9th World Congress on Structural and Multidisciplinary Optimization, 2011

    Details
  7. Stability-Constrained Aerodynamic Shape Optimization of Flying Wings

    C. A. Mader, and J. R. R. A. Martins

    Proceedings of the CASI Conference, 2011

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2010

  1. Stability-Constrained Aerodynamic Shape Optimization of a Flying Wing Configuration

    C. A. Mader, and J. R. R. A. Martins

    Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, 2010

    Details
  2. Parallel Solution Methods for Aerostructural Analysis and Design Optimization

    G. J. Kennedy, and J. R. R. A. Martins

    Proceedings of the 13^th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, 2010

    Details
  3. Reducing Aviation’s Environmental Impact Through Large Aircraft For Short Ranges

    G. K. W. Kenway, R. Henderson, J. E. Hicken, N. B. Kuntawala, D. W. Zingg, J. R. R. A. Martins, McKe, and G. Ross

    Proceedings of the 48th AIAA Aerospace Sciences Meeting and Exhibit, 2010

    doi:10.2514/6.2010-1015

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  4. A CAD-Free Approach to High-Fidelity Aerostructural Optimization

    G. K. Kenway, G. J. Kennedy, and J. R. R. A. Martins

    Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, (AIAA 2010-9231), 2010

    doi:10.2514/6.2010-9231

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  5. A New Approach to Multidisciplinary Design Optimization via Internal Decomposition

    A. B. Lambe, and J. R. R. A. Martins

    Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2010

    doi:10.2514/6.2010-9325

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  6. Topology Optimization Using a Level Set Method with an Arbitrary Structured Mesh

    K. A. James, and J. R. R. A. Martins

    6th AIAA Multidisciplinary Design Optimization Specialist Conference, 2010

    Details
  7. Application of Robust Control Design Techniques to the Aeroservoelastic Design Optimization of a Very Flexible UAV Wing

    S. Haghighat, H. H. T. Liu, and J. R. R. A. Martins

    Proceedings of the 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, 2010

    Details

2009

  1. Conceptual Design and Optimization of Environmentally-Friendly Aircraft

    R. Henderson, and J. R. R. A. Martins

    Proceedings of the 2009 SAE AeroTech Congress and Exhibition, 2009

    Details
  2. A Discrete Adjoint Formulation for Stability Derivatives Using the ADjoint Approach

    C. A. Mader, and J. R. R. A. Martins

    Proceedings of the CASI Conference, 2009

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2008

  1. A Framework for High-Fidelity Aerostructural Optimization of Aircraft Configurations

    C. A. Mader, G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the International Conference on System Simulation and Scientific Computing, 2008

    Details
  2. A Configurable B-Spline Parametrization Method for Structural Optimization of Wing Boxes

    A. T. Yu, and J. R. R. A. Martins

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

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  3. Towards High-Fidelity Aerostructural Optimization Using a Coupled ADjoint Approach

    C. A. Mader, G. Kenway, and J. R. R. A. Martins

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

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  4. Aerostructural Optimization of Aircraft Structures Using Asymmetric Subspace Optimization

    G. Kennedy, J. R. R. A. Martins, and J. S. Hansen

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

    Details
  5. Progressive Validity Trust Region Optimization Using a Kriging Metamodel

    Q. Thomson, and J. R. R. A. Martins

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

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  6. Modeling and Simulation of Flexible UAVs with Large Aspect Ratio

    S. Haghighat, H. H. T. Liu, and J. R. R. A. Martins

    Proceedings of the International Conference on System Simulation and Scientific Computing, 2008

    Details
  7. pyACDT: An Object-Oriented Framework for Aircraft Design Modelling and Multidisciplinary Optimization

    R. E. Perez, and J. R. R. A. Martins

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

    Details
  8. Multidisciplinary Design Optimization of Airframe and Engine for Emissions Reduction

    R. E. Perez, R. Henderson, and J. R. R. A. Martins

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

    Details
  9. Aerostructural Optimization of Non-Planar Lifting Surface Configurations

    R. E. Perez, P. W. Jansen, and J. R. R. A. Martins

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

    Details
  10. Reconfigurable Semi-Analytic Sensitivity Methods and MDO Architectures within the \piMDO Framework

    C. J. Marriage, and J. R. R. A. Martins

    Proceedings of the 12^th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

    doi:10.2514/6.2008-5956

    Details
  11. Structural Topology Optimization for Multiple Load Cases While Avoiding Local Minima

    K. A. James, J. S. Hansen, and J. R. R. A. Martins

    Proceedings of the 4th AIAA Multidisciplinary Design Optimization Specialist Conference, 2008

    Details
  12. Aerostructural Shape Optimization of Wind Turbine Blades Considering Site-Specific Winds

    G. K. W. Kenway, and J. R. R. A. Martins

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

    doi:10.2514/6.2008-6025

    Details
  13. Three-Dimensional Structural Topology Optimization of an Aircraft Wing Using Level Set Methods

    K. James, and J. R. R. A. Martins

    Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2008

    Details

2007

  1. Subspace Optimization of Multidisciplinary Systems Using Coupled Post-Optimality Sensitivity Analysis

    J. R. R. A. Martins, and I. R. Chittick

    Proceedings of the 7th World Congress on Structural and Multidisciplinary Optimization, 2007

    Details
  2. An Object-Oriented Framework for Multidisciplinary Design Optimization

    J. R. R. A. Martins, and C. Marriage

    Proceedings of the 3rd AIAA Multidisciplinary Design Optimization Specialist Conference, 2007

    Details
  3. Towards Aerodynamic Shape Optimization of an Oblique Wing Using the ADjoint Approach

    C. A. Mader, J. R. R. A. Martins, and A. C. Marta

    Proceedings of the CASI Conference, 2007

    Details
  4. Aerodynamic Shape Optimization of an Oblique Wing Using the ADjoint Approach

    C. A. Mader, A. C. Marta, and J. R. R. A. Martins

    Proceedings of the 15th Conference of the CFD Society of Canada, 2007

    Details
  5. Structural Optimization of a Wing Box Using B-Spline Parametrization

    A. T. Yu, and J. R. R. A. Martins

    Proceedings of the CASI Conference, 2007

    Details
  6. A New Subspace Optimization Method for Aero-Structural Design

    I. R. Chittick, and J. R. R. A. Martins

    Proceedings of the 3rd AIAA Multidisciplinary Design Optimization Specialist Conference, 2007

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  7. Towards Aircraft Design Using an Automatic Discrete Adjoint Solver

    C. A. Mader, J. R. R. A. Martins, and A. C. Marta

    Proceedings of the 18th AIAA Computational Fluid Dynamics Conference, 2007

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2006

  1. Comparison of MDO Architectures within a Universal Framework

    N. P. Tedford, and J. R. R. A. Martins

    Proceedings of the 2nd AIAA Multidisciplinary Design Optimization Specialist Conference, 2006

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  2. ADjoint: An Approach for Rapid Development of Discrete Adjoint Solvers

    J. R. R. A. Martins, C. A. Mader, and J. J. Alonso

    Proceedings of the 11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2006

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  3. On the Common Structure of MDO Problems: A Comparison of Architectures

    N. P. Tedford, and J. R. R. A. Martins

    Proceedings of the 11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2006

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  4. An Automated Approach for Developing Discrete Adjoint Solvers

    J. R. R. A. Martins, J. J. Alonso, and d. W. E. van

    Proceedings of the 2nd AIAA Multidisciplinary Design Optimization Specialist Conference, 2006

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2005

  1. On Structural Optimization Using Constraint Aggregation

    J. R. R. A. Martins, and N. M. K. Poon

    Proceedings of the 6th World Congress on Structural and Multidisciplinary Optimization, 2005

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  2. Efficient Coupled-Sensitivity Analysis Methods for Aero-Structural Optimization

    A. T. Yu, and J. R. R. A. Martins

    Proceedings of the CASI Aircraft Design and Development Symposium, 2005

    Details
  3. Variable Complexity Methods Applied to Airfoil Optimization

    P. Thokala, and J. R. R. A. Martins

    Proceedings of the CASI Aircraft Design and Development Symposium, 2005

    Details
  4. Adaptive Constraint Aggregation for Structural Optimization Using Adjoint Sensitivities

    N. M. K. Poon, and J. R. R. A. Martins

    Proceedings of the CASI Aircraft Design and Development Symposium, 2005

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2004

  1. pyMDO: A Framework for High-Fidelity Multi-Disciplinary Optimization

    J. J. Alonso, P. LeGresley, d. W. E. van, J. R. R. A. Martins, and J. J. Reuther

    Proceedings of the 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 2004

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2003

  1. High-Fidelity Aero-Structural Design Using a Parametric CAD-Based Model

    J. J. Alonso, J. R. R. A. Martins, J. J. Reuther, and R. Haimes

    Proceedings of the 16th AIAA Computational Fluid Dynamics Conference, 2003

    doi:10.2514/6.2003-3429

    Details
  2. Aero-Structural Optimization of Aircraft Configurations Using Coupled-Sensitivity Analysis

    J. R. R. A. Martins, J. J. Alonso, and P. LeGresley

    Proceedings of the SIAM Conference on Computational Science and Engineering, 2003

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2002

  1. Complete Configuration Aero-Structural Optimization Using a Coupled Sensitivity Analysis Method

    J. R. R. A. Martins, J. J. Alonso, and J. J. Reuther

    Proceedings of the 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, 2002

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  2. High-Fidelity Aero-Structural Design Optimization of a Supersonic Business Jet

    J. R. R. A. Martins, J. J. Alonso, and J. J. Reuther

    Proceedings of the 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2002

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2001

  1. The Connection Between the Complex-Step Derivative Approximation and Algorithmic Differentiation

    J. R. R. A. Martins, P. Sturdza, and J. J. Alonso

    Proceedings of the 39th AIAA Aerospace Sciences Meeting, 2001

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  2. Aero-Structural Wing Design Optimization Using High-Fidelity Sensitivity Analysis

    J. R. R. A. Martins, J. J. Alonso, and J. J. Reuther

    Proceedings of the CEAS Conference on Multidisciplinary Aircraft Design and Optimization, 211–226, 2001

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  3. Fortran to Python Interface Generator with an Application to Aerospace Engineering

    P. Peterson, J. R. R. A. Martins, and J. J. Alonso

    Proceedings of the 9th International Python Conference, 2001

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2000

  1. An Automated Method for Sensitivity Analysis Using Complex Variables

    J. R. R. A. Martins, I. M. Kroo, and J. J. Alonso

    Proceedings of the 38th AIAA Aerospace Sciences Meeting, 2000

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1999

  1. A Coupled Aero-Structural Optimization Method for Complete Aircraft Configurations

    J. Reuther, J. J. Alonso, J. R. R. A. Martins, and S. C. Smith

    Proceedings of the 37th AIAA Aerospace Sciences Meeting and Exhibit, 1999

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2021

  1. Engineering Design Optimization

    J. R. R. A. Martins, and A. Ning

    2021

    doi:10.1017/9781108980647

    Details

2019

  1. Passive Aeroelastic Tailoring

    B. Smith, T. R. Brooks, M. Leader, T. W. Chin, G. J. Kennedy, J. R. R. A. Martins, and C. E. S. Cesnik

    (CR-2019-XXXXXX), 2019

    Details
  2. DAFoam Multidisciplinary Design Optimization Setup

    P. He, C. A. Mader, J. R. R. A. Martins, and K. J. Maki

    2019

    doi:10.17632/cg4n68bm9v

    Details
  3. mSANN model benchmarks

    M. A. Bouhlel, and J. R. R. A. Martins

    2019

    doi:10.17632/ngpd634smf.1

    Details
  4. CFD discrete adjoint benchmarks

    G. K. W. Kenway, C. A. Mader, P. He, and J. R. R. A. Martins

    2019

    doi:10.17632/w4hsj8wzm8

    Details

2017

  1. Advances and Trends in Optimization with Engineering Applications

    J. R. R. A. Martins

    249–257, 2017

    doi:10.1137/1.9781611974683.ch19

    Details
  2. High-fidelity Multidisciplinary Design Optimization of Aircraft Configurations

    J. R. R. A. Martins, G. K. W. Kenway, D. Burdette, E. Jonsson, and G. J. Kennedy

    (2017–219647), 2017

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2016

  1. Multidisciplinary Design Optimization of Aircraft Configurations—Part 2: High-fidelity aerostructural optimization

    J. R. R. A. Martins, G. K. W. Kenway, and T. R. Brooks

    2016

    Details
  2. High-Fidelity Aerostructural Optimization of the Airbus XRF1 Aircraft Configuration

    G. K. Kenway, and J. R. R. A. Martins

    2016

    Details
  3. The Metabook of Aircraft Design

    J. R. R. A. Martins

    2016

    Details
  4. High-fidelity Aerostructural Optimization Considering Manufacturing Cost

    T. R. Brooks, , and R. R. A. M. Joaquim

    2016

    Details
  5. Encyclopedia of Aerospace Engineering

    J. R. R. A. Martins

    Green Aviation75–79, 2016

    doi:10.1002/9780470686652.eae1007

    Details
  6. Multidisciplinary Design Optimization of Aircraft Configurations—Part 1: A modular coupled adjoint approach

    J. R. R. A. Martins, and J. T. Hwang

    2016

    Details

2015

  1. AIAA ADODG Case 5: CRM Wing-Body-Tail Optimization at Flight Reynolds Number

    G. K. W. Kenway, and J. R. R. A. Martins

    2015

    Details
  2. Aerostructural Analysis of the Airbus XRF1 Aircraft Configuration

    G. K. W. Kenway, and J. R. R. A. Martins

    2015

    Details
  3. Handbook of Clean Energy Systems

    N. Xue, W. Du, J. R. R. A. Martins, and W. Shyy

    5 : Energy Storage2849–2864, 2015

    doi:10.1002/9781118991978

    Details

2014

  1. A Comparison of Metallic, Composite and Nanocomposite Optimal Transonic Transport Wings

    G. J. Kennedy, G. K. Kenway, and J. R. R. A. Martins

    2014

    Details

2010

  1. The Future of Multidisciplinary Design Optimization: Advancing the Design of Complex Engineered Systems.

    T. Simpson, and J. R. R. A. Martins

    2010

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2009

  1. Aerodynamic Design of a 10 kW Vertical Axis Wind Turbine

    G. K. W. Kenway, and J. R. R. A. Martins

    2009

    Details

2008

  1. Vale Experimental Towed Platform—Aerodynamic Shell Design

    P. Jansen, and J. R. R. A. Martins

    2008

    Details

2007

  1. A Review of a Wind Tunnel Test Report

    J. R. R. A. Martins

    2007

    Details

2005

  1. C-Class Airfoil Analysis, Part 1

    J. R. R. A. Martins

    2005

    Details
  2. C-Class Airfoil Analysis, Part 2

    J. R. R. A. Martins

    2005

    Details

2002

  1. A Coupled-Adjoint Method for High-Fidelity Aero-Structural Optimization

    J. R. R. A. Martins

    2002

    Details

1997

  1. Drag Reduction of Staggered Supersonic Wings

    J. R. R. A. Martins

    1997

    Details

1995

  1. Self-Similar Solutions for the Plane Turbulent Jet

    J. R. R. A. Martins

    1995

    Details

1994

  1. Front Fuselage Structure of an Advanced Air Superiority Fighter

    J. R. R. A. Martins

    1994

    Details