Improvement of Helicopter Rotor Blade-Vortex Interaction Noise Prediction Using a Rotor Wake Roll-Up Model
1st Joint aeroacoustics conference ; 1995 ; Munich; Germany
01.01.1995
9 pages
In 2 vols; Also known as the 16th AIAA aeroacoustics conference
Aufsatz (Konferenz)
Englisch
aeroacoustics , CEAS , AIAA
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Blade-Vortex Interaction Noise Prediction Using a Rotor Wake Roll-Up Model
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