Comparison of Computed and Measured Vortex Evolution for a UH-60A Rotor in Forward Flight
Author:
Affiliation:
1. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3160
Reference20 articles.
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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3. Effect of Fuselage and Wind Tunnel Wall on Full-Scale UH-60A Rotor Tip Vortex Prediction;34th AIAA Applied Aerodynamics Conference;2016-06-10
4. Performance and Physics of a S-76 Rotor in Hover With Non-Contiguous Hybrid Methodologies;54th AIAA Aerospace Sciences Meeting;2016-01-02
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