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Title	Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients /
Format	online resource
Internet Access	https://purl.fdlp.gov/GPO/gpo52217
Author	Sanders, Bobby W., author.
Published	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.

SuDoc Number	NAS 1.60:1531
Item Number	0830-H-15 (online)
Description	1 online resource (iii, 98 pages) : illustrations.
Content Type	text
Series	(NASA technical paper ; 1531.)
General Note	Title from title screen (viewed Sept. 22, 2014).
	"January 1980."
	"Performing organization, Lewis Research Center"--Technical report documentation page.
Bibliography	Includes bibliographical references (pages 27-28).
Subject - LC	Airplanes -- Turbojet engines -- Air intakes.
	Airplanes -- Motors -- Valves.
Added Entry	United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, issuing body.
	Lewis Research Center, author.
Linking Field	Print version: Sanders, Bobby W. Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients (OCoLC)7959956
URL	http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19800005866.pdf

Holdings	All items

OCLC Number	(OCoLC)761221787
CGP Record Link	https://catalog.gpo.gov:443/F/?func=direct&doc_number=000935445&local_base=GPO01PUB
System Number	000935445

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