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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 / Bobby W. Sanders.

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Series Information

NASA technical paper

Record details

  • Physical Description: 1 online resource (iii, 98 pages) : illustrations.
  • Publisher: Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.

Content descriptions

General Note:
Title from title screen (viewed Sept. 22, 2014).
"January 1980."
"Performing organization, Lewis Research Center"--Technical report documentation page.
Bibliography, etc. Note:
Includes bibliographical references (pages 27-28).
Funding Information Note:
Sponsored by National Aeronautics and Space Administration 505-04
E-9467
Subject: Airplanes > Turbojet engines > Air intakes.
Airplanes > Motors > Valves.

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