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 /

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Bibliographic Details
Author / Creator:	Sanders, Bobby W., author.
Imprint:	Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
Description:	1 online resource (iii, 98 pages) : illustrations.
Language:	English
Series:	NASA technical paper ; 1531 NASA technical paper ; 1531.
Subject:	Airplanes -- Turbojet engines -- Air intakes. Airplanes -- Motors -- Valves. Airplanes -- Motors -- Valves. Airplanes -- Turbojet engines -- Air intakes.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/10292775

Hidden Bibliographic Details
Other authors / contributors:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, issuing body. Lewis Research Center, author.
Notes:	Title from title screen (viewed Sept. 22, 2014). "January 1980." "Performing organization, Lewis Research Center"--Technical report documentation page. Includes bibliographical references (pages 27-28). Sponsored by National Aeronautics and Space Administration 505-04 E-9467
Other form:	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
GPO item no.:	0830-H-15 (online)
Govt.docs classification:	NAS 1.60:1531

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