Computational Modeling of Hovering Rotor and Wake Aerodynamics
Author:
Affiliation:
1. U.S. Army Aviation and Missile Command, Moffett Field, California 94035-1000
2. NASA Ames Research Center, Moffett Field, California 94035-1000
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.3024
Reference18 articles.
1. Flowfield of a lifting rotor in hover - A Navier-Stokes simulation
2. Flowfield Analysis of Modern Helicopter Rotors in Hover by Navier‐Stokes Method
3. Evaluation of a Navier‐Stokes Analysis Method for Hover Performance Prediction
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