Meshless Large-Eddy Simulation of Propeller–Wing Interactions with Reformulated Vortex Particle Method
The vortex particle method (VPM) has gained popularity in recent years due to a growing need to predict complex aerodynamic interactions during the preliminary design of electric multirotor aircraft. However, VPM is known to be numerically unstable when vortical structures break down close to the tu...
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Veröffentlicht in: | Journal of aircraft 2024-05, Vol.61 (3), p.811-827 |
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Sprache: | eng |
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