Induced inflow velocity and blade surface pressure measurements for a helicopter model in forward flight. Volume 1, Advance ratio of 0.37, thrust coefficient of 0.0081 and hover tip speed of 710 ft/sec [microform] / Joe W. Elliott [and others]

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Bibliographic Details
Corporate Authors:	United States. Army Aviation Research and Technology Activity, Langley Research Center
Other Authors:	Elliott, Joe W.
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : [St. Louis, Mo.] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, Aviation R&T Activity, [1992]
Series:	AVSCOM technical report ; 92-B-3. NASA technical memorandum ; 104224.
Subjects:	Rotors (Helicopters) > Aerodynamics. Laser Doppler velocimeter.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:104224
NAS 1.15:104224	Restricted Place a Hold