Helicopter rotor blade computation in unsteady flows using moving overset grids
Author:
Affiliation:
1. Sterling Software, Moffett Field, California 94035-1000
2. U.S. Army Aeroflightdynamics Directorate, Moffett Field, California 94035-1000
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46902
Reference22 articles.
1. Flowfield of a lifting rotor in hover - A Navier-Stokes simulation
2. TURNS: A Free-Wake Eule/Navier-Stokes Numerical Method for Helicopter Rotors
3. An Euler solver for calculating the flowfield of a helicopter rotor in hover and forward flight
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