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- W2334606541 abstract "A coupled CFD-CSD solver is used to simulate the aerodynamics of a flexible flapping wing. The CFD solver is a compressible RANS solver. The free general-purpose multibody dynamics solver MBDyn is used as the structural solver after an extension to take into account non linear shell straining, making it possible to analyze plates with large deformations. Validation of the two codes for flapping wings/plates is carried out independently. The solvers are then coupled and validated against prior experiments and analysis on a spanwise flexible wing at Re = 30,000. It is observed that due to flexibility, the average chordwise propulsive force, CT increases by 47% as a result of increase in plunge amplitude, effective angle of attack and leading edge suction towards the outer sections as compared to for a rigid wing. Additionally, the flexible wing has higher 3D flow. Then, a chordwise flexible root flapping wing is analyzed using the solver at Re = 10,000. As a result of the flexibility, camber is induced in the wing as it flaps. Highly 3D flow was observed with the strength of the vortices increasing from root to tip. Due to camber in the wing, the resultant force is vectored more in the chordwise direction as compared to for rigid wings, which results in higher thrust. The average CT increased by 25% and average CL increased by 10%. The current work demonstrates the capability of an aeroelastic solver to characterize the flowfield of a flexible flapping wing MAV in 3D." @default.
- W2334606541 created "2016-06-24" @default.
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- W2334606541 date "2012-04-23" @default.
- W2334606541 modified "2023-10-16" @default.
- W2334606541 title "CFD-CSD Coupled Aeroelastic Analysis of Flexible Flapping Wings for MAV Applications: Methodology Validation" @default.
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- W2334606541 doi "https://doi.org/10.2514/6.2012-1636" @default.
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