F-111A airplane in-flight inlet pressure fluctuations for engine compressor surge, discussing average turbulence factor
Analysis of in-flight pressure fluctuations leading to engine compressor surge in an F-111A airplane for Mach numbers to 2.17
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH ; 1970 ; SAN DIEGO, CA
1970-06-01
Conference paper
No indication
English