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
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
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 98
Subjects: Airplanes -- Turbojet engines -- Air intakes; Airplanes -- Motors -- Valves
Notes: "Lewis Research Center."

"January 1980"--Cover

Includes bibliographical references