Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet
By: Bobby W. Sanders
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Lewis Research Center
Series: NASA technical paper -- 1532
Publisher: NASA, 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: 78
Subjects: Airplanes -- Turbojet engines -- Air intakes
Notes: "Lewis Research Center."

"January 1980"--Cover

Includes bibliographical references