Parametric tip effects for conformable rotor applications [microform] / Wayne R. Mantay, William T. Yeager, Jr.

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Bibliographic Details
Main Author:	Mantay, Wayne R.
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, United States. Army Aviation Research and Development Command, Army Research and Technology Laboratories (U.S.), Structures Laboratory (U.S.)
Other Authors:	Yeager, William T.
Other title:	Tip effects for conformable rotor applications. Conformable rotor applications.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, 1983.
Series:	AVRADCOM technical report ; 83-B-4 NASA technical memorandum ; 85682.
Subjects:	Helicopter rotors > Wind tunnel tests. Rotor blades > Wind tunnel tests. Aeroelasticity. Wind tunnel tests. Aerodynamic configurations.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:85682
NAS 1.15:85682	Restricted Place a Hold