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
By: Bobby W. Sanders
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Lewis Research Center
Series: NASA technical paper -- 1531; NASA technical paper -- 1531.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office
Published: 1980
Place of publication: Washington, D.C
Language: eng
Number of pages: 98
Subjects: Airplanes; Turbojet engines; Air intakes; Motors; Valves; Aerodynamic stability; Bypasses; Propulsion system performance; Supersonic inlets; Wind tunnel stability tests
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