Turbulent base flowfields in multinozzle configurations, considering adiabatic flow and determining base pressure distribution from reverse jet impingement
A theory for base pressures on multinozzle rocket configurations
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 5TH, U.S. AIR FORCE ACADEMY ; 1969 ; COLORADO SPRINGS, CO
1970-04-01
Miscellaneous
No indication
English
Experimental Study of a Multinozzle Combustor at Elevated Pressures
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