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Author

Title Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities / Laurence D. Leavitt and James R. Burley II.

Imprint

[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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Connect to http://purl.access.gpo.gov/GPO/LPS122510

Location	Call No.	OPAC Message	Status
Axe Federal Documents Online	NAS 1.60:2519	---	Available

Description	1 online resource (106 pages).
	text txt rdacontent
	computer c rdamedia
	online resource cr rdacarrier
Series	NASA technical paper ; 2519
	NASA technical paper ; 2519.
Bibliography	Includes bibliographical references (pages 14-15).
Subject	Jet nozzles.
	Jet planes -- Thrust reversers -- Testing.
	Jet nozzles. (OCoLC)fst00982414
	Jet planes -- Thrust reversers -- Testing. (OCoLC)fst00982448
	Nozzle geometry.
	Static tests.
	Thrust reversal.
	Wind tunnel tests.
Added Author	Burley, James R.
	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Other Form:	Microform version: Leavitt, Laurence D. Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities. (OCoLC)24956419
Gpo Item No.	0830-H-15 (online)
Sudoc No.	NAS 1.60:2519