Solution method for a hovering helicopter rotor using the Euler equations
Author:
Affiliation:
1. MIT, Cambridge, MA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-436
Reference13 articles.
1. Roberts, T.W., and Murman, E.M. "A Computational Method for Helicopter Vortex Wakes," AIAA paper 84-1554,1984.
2. Subsonic and Transonic Potential Flow over Helicopter Rotor Blades
3. Computation of flow around wings based on the Euler equations
4. Computation of simple three-dimensional wing-vortex interaction in transonic flow
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