Experimental blade vortex interaction noise characteristics of a utility helicopter at 1/4 scale /

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Bibliographic Details
Main Author:	Conner, David A. (David Alan), 1956-
Corporate Authors:	United States. Army Aviation Research and Development Command, Langley Research Center
Other Authors:	Hoad, Danny R.
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : [St. Louis, Mo.] : National Aeronautics and Space Administration, Langley Research Center ; [United States Army Aviation Research and Development Command], [1984]
Series:	NASA technical memorandum ; 84653. AVSCOM technical memorandum ; 83-B-1.
Subjects:	Acoustical engineering. Rotors (Helicopters) Blade slap noise. Blade-vortex interaction. Rotary wings. UH-1 helicopter. Vortices. Wind tunnels.

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Call Number:	NAS 1.15: 84653
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