Skin Friction Predictions over a Hovering Tilt-Rotor Blade Using OVERFLOW2
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3186
Reference40 articles.
1. Revolutionary Physics-Based Design Tools for Quiet Helicopters
2. Overset Solution Adaptive Grid Approach Applied to Hovering Rotorcraft Flows
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