Navier-Stokes calculations for the vortex wake of a rotor in hover
Author:
Affiliation:
1. NASA, Langley Research Center, Low-Speed Aerodynamics Div., Hampton, VA
2. U.S. Army, Aeromechanics Laboratory, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1676
Reference10 articles.
1. On the application of the integral invariants and decay laws of vorticity distributions
2. Numerical solution of viscous flow in unbounded fluid
3. Approximate boundary condition procedure for the two-dimensional numerical solution of vortex wakes
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1. Modern helicopter rotor aerodynamics;Progress in Aerospace Sciences;2001-07
2. Free-wake analysis of a rotor in hover;19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference;1987-06-08
3. Recent developments in rotary-wing aerodynamic theory;AIAA Journal;1986-08
4. Navier-Stokes calculations for unsteady three-dimensional vortical flows in unbounded domains;AIAA Journal;1985-06
5. A method for modeling finite-core vortices in wake-flow calculations;22nd Aerospace Sciences Meeting;1984-01-09
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