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Prediction of Maximum Flapping Frequency of a Flapping Wing Using Unsteady Vortex Lattice Method and Finite Element Method

Category √
Sub-Category √
ICSV
Year √
2025
Author √
Co-Author
Keywords
Flapping
Mechanism
UVLM
Status √
Published
Files
ICSV_2025_Prediction of Maximum Flapping Frequency for a Flapping Mechanism Using Unsteady Vortex Lattice Method and Finite Element Method.pdf
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Citation
Lee, S.-G., Yang, H.-H., and Han, J.-H., 2025, “Prediction of Maximum Flapping Frequency of a Flapping Wing Using Unsteady Vortex Lattice Method and Finite Element Method,” 31st International Congress on Sound and Vibration, Incheon, Republic of Korea, Jul. 6-11, 291.