Title: 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
Subjects: Airplanes, Turbojet engines, Air intakes, Motors, Valves, Aerodynamic stability, Bypasses, Propulsion system performance, Supersonic inlets, Wind tunnel stability tests