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

An edition of 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 (1980)

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

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Publish Date

1980

Publisher

NASA, Scientific and Technical Information Office,For sale by the National Technical Information Service]

Language

eng

Pages

Description:

subjects: Air intakes, Airplanes, Turbojet engines