Flowfield Measurements to Understand Effect of Wake Behavior on Rotor Performance
Author:
Affiliation:
1. University Affiliated Research Center
2. U.S. Army Research, Development and Engineering Command
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4237
Reference20 articles.
1. The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor Performance
2. Rotor Tip Vortex Geometry Measurements Using the Wide‐Field Shadowgraph Technique
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3. Rotor Wake Investigation Under Autorotation Condition in Water Tunnel;IEEE Access;2023
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