Helicopter impulsive noise ; theoretical and experimental status [microform] / F.H. Schmitz and Y.H. Yu.

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Bibliographic Details
Main Author:	Schmitz, F. H.
Corporate Authors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, United States. Army Aviation Research and Development Command, Ames Research Center, Aeromechanics Laboratory, Army Research and Technology Laboratories (U.S.)
Other Authors:	Yu, Yung H.
Other title:	Impulsive noise.
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, 1983.
Series:	AVRADCOM technical report ; 83-A-2 NASA technical memorandum ; 84390.
Subjects:	Helicopters > Noise. Aerodynamic noise. Impulse noise. Noise. Vortices > Noise. Rotor blades > Noise. Tail helicopter rotors > Noise. Mathematical models. Helicopters.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:84390
NAS 1.15:84390	Restricted Place a Hold