Fast Computational Aeroelastic Analysis of Helicopter Rotor Blades
Author:
Affiliation:
1. Cranfield University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1044
Reference17 articles.
1. Low-Speed Aerodynamics
2. Applications of the unsteady vortex-lattice method in aircraft aeroelasticity and flight dynamics
3. Three-dimensional flow structures and vorticity control in fish-like swimming
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