Prediction of Wake Structure and Induced Velocity of a Helicopter Rotor in the Vortex Ring State using a Vortex Particle Method

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Publisher
Asian-Australian Rotorcraft Forum
Issue Date
2014-12-18
Language
English
Citation

3rd Asian-Australian Rotorcraft Forum (ARF)

URI
http://hdl.handle.net/10203/193287
Appears in Collection
AE-Conference Papers(학술회의논문)
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