Conference Paper
Investigating the Influence of an Inboard Propeller’s Vertical Offset on a Trailing Wing’s Lift and Drag Distributions
S. S. Chauhan, d. S. G. Padovany, G. L. O. Halila, J. R. R. A. Martins, and J. L. F. Azevedo
Proceedings of the 34th International Council of the Aerospace Sciences, (ICAS2024_0124), 2024
Propeller-wing interaction has been a topic of investigation since the dawn of aviation. Surprisingly, however, there are few published studies showing how changing a tractor propeller’s vertical offset affects a trailing wing’s lift and drag distributions. In this work, we investigate this for a rectangular wing with an inboard propeller using steady Reynolds-averaged Navier–Stokes computational fluid dynamics and an actuator-disk approach. We present results for two angles of attack and a range of propeller-wing vertical offsets for both inboard-up and outboard-up propeller rotation. We include plots for spanwise sectional lift and drag coefficient distributions, integrated lift and drag coefficients, lift-to-drag ratios, and chordwise sectional pressure-coefficient distributions. The results show that changing the propeller-wing vertical offset can significantly change a trailing wing’s lift and drag distributions, which strongly depend on the direction of the vertical offset.