Jet engine compressor stalls in-flight investigation up to Mach 2 on F-111A by pressure sensors, noting steady state distortion role
The flight investigation of pressure phenomena in the air intake of an F-111A airplane.
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE ; 1969 ; COLORADO SPRINGS, COLO.
1969-06-01
Conference paper
No indication
English