MPhys

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MPhys is a multiphysics analysis and optimization software library that facilitates the development of high- and mixed-fidelity models in OpenMDAO. MPhys development is led by NASA with contributions from the MDO Lab and other academic and government institutions. MPhys is available under an open-source license: github.com/OpenMDAO/mphys

    Publications from the MDO Lab that used MPhys

    1. A Proposed Benchmark Model for Practical Aerostructural Optimization of Aircraft Wings

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

      AIAA SciTech Forum, 2024

      doi:10.2514/6.2024-2775

      Details

    2. Coupled Aeropropulsive Design Optimization of an Over-Wing Nacelle Configuration

      M. A. S. Abdul-Kaiyoom, A. Yildirim, , and R. R. A. M. Joaquim

      AIAA SciTech Forum, 2023

      doi:10.2514/6.2023-0327

      Details

    3. RANS-Based Multipoint Aeropropulsive Design Optimization of an Over-Wing Nacelle Configuration

      M. A. S. Abdul-Kaiyoom, A. Yildirim, and J. R. R. A. Martins

      AIAA Aviation Forum, 2023

      doi:10.2514/6.2023-3588

      Details

    4. Geometrically Nonlinear High-fidelity Aerostructural Optimization Including Geometric Design Variables

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

      AIAA Aviation Forum, 2023

      doi:10.2514/6.2023-3316

      Details

    5. Combined systems packaging and aerodynamic shape optimization of a full aircraft configuration

      H. M. Hajdik, B. Pacini, A. Yildirim, B. J. Brelje, and J. R. R. A. Martins

      AIAA Aviation Forum, 2023

      doi:10.2514/6.2023-3589

      Details

    6. Advancements in Coupled Aeropropulsive Design Optimization for High-Bypass Turbofan Engines

      A. H. R. Lamkin, A. Yildirim, J. R. R. A. Martins, and N. A. Wukie

      AIAA Aviation Forum, 2023

      doi:10.2514/6.2023-3591

      Details

    7. Understanding Distributed Propulsion on the NASA Tiltwing Concept Vehicle with Aerodynamic Shape Optimization

      B. Pacini, M. Prajapati, K. Duraisamy, J. R. R. A. Martins, and P. He

      AIAA Scitech Forum 2023, 2023

      doi:10.2514/6.2023-0143

      Details

    8. Multipoint Aerostructural Optimization for Urban Air Mobility Vehicle Design

      B. Pacini, M. Prajapati, K. Duraisamy, J. R. R. A. Martins, and P. He

      AIAA Scitech Forum 2023, 2023

      doi:10.2514/6.2023-0326

      Details

    9. Towards Mixed-Fidelity Aero-Structural-Acoustic Optimization for Urban Air Mobility Vehicle Design

      B. Pacini, M. Prajapati, K. Duraisamy, J. R. R. A. Martins, and P. He

      AIAA Aviation Forum, 2023

      doi:10.2514/6.2023-3905

      Details

    10. Aerodynamic shape optimization of an electric aircraft motor surface heat exchanger with conjugate heat transfer constraint

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

      International Journal of Heat and Mass Transfer, 189122689, 2022

      doi:10.1016/j.ijheatmasstransfer.2022.122689

      Details

    11. CFD-based shape optimization of a plate-fin heat exchanger

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

      AIAA AVIATION 2022 Forum, 2022

      doi:10.2514/6.2022-3930

      Details

    12. Coupled aeropropulsive analysis and optimization of a high bypass turbofan engine

      A. H. Lamkin, A. Yildirim, and J. R. R. A. Martins

      33rd Congress of the International Council of the Aeronautical Sciences, 2022

      Details

    13. Boundary Layer Ingestion Benefit for the STARC-ABL Concept

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

      Journal of Aircraft, 59(4):896–911, 2022

      doi:10.2514/1.C036103

      Details

    14. A Nonlinear Schur Complement Solver for CFD-Based Multidisciplinary Models

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

      Eleventh International Conference on Computational Fluid Dynamics, 2022

      Details

    15. 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

    16. 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

    Tags:

    MDO
    open mdao