HELICOPTER MODEL ROTOR-BLADE VORTEX INTERACTION IMPULSIVE NOISE: SCALABILITY AND PARAMETRIC VARIATIONS.

被引：0
|
作者：
Boxwell, D.A. [1 ]
Schmitz, F.H. [1 ]
Splettstoesser, W.R. [1 ]
Schultz, K.J. [1 ]
机构：
[1] U. S. Army Aviation Research &, Technology Activity, Ames Research, Cent, Moffett Field, CA, USA, U. S. Army Aviation Research & Technology Activity, Ames Research Cent, Moffett Field, CA, USA
来源：
| 1600年 / 32期
关键词：
All Open Access; Green;
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摘要：
Helicopters
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