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.

Description
Item Description:	"August 1983." STAR Subject category 39.
Physical Description:	29 pages : illustrations ; 28 cm.
Bibliography:	References: pages 13-14.
Access:	Unclassified; unlimited.
Funding Information Note:	Project no.
Type of Report and Period Covered Note:	Technical memorandum.

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