Euler Calculations of Unsteady Interaction of Advancing Rotor with a Line Vortex
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49095
Reference25 articles.
1. Numerical simulation of tip vortices of wings in subsonic and transonic flows
2. An experimental study of rotor-vortex interactions
3. Navier-Stokes simulations of blade-vortex interaction using high-order accurate upwind schemes
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