A review of the accomplishments achieved under this AFOSR contract is presented. Among the most notable are: (1) the development and demonstration of a fully-coupled rocket nozzle code (FULLNOZ) which, in calculating nozzle flow properties, couples the effects of nonequilibrium chemistry, gas/particle thermal and dynamic nonequilibrium, turbulent mixing across streamtubes and turbulent wall boundary layers and (2) the development of a phenomeno-logical model for the interpretation of IR radiation data from subscale liquid propellant rocket motor plumes; the model accounts for the effects of unburned fuel on rocket nozzle and after-burning plume properties.
Chemical Kinetic/Gas Dynamic/Particle Interactions in Rocket Nozzle and Exhaust Plume Flows
1976
11 pages
Report
No indication
English
Combustion & Ignition , Exhaust plumes , Rocket nozzles , Liquid propellant rocket engines , Infrared radiation , Afterburning , Computerized simulation , Computer programs , Gas dynamics , Nonequilibrium flow , Reaction kinetics , Gases , Particles , Interactions , Turbulent flow , Turbulent boundary layer , FULLNOZ computer program
Problems of rocket exhaust plume interactions.
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|Rocket exhaust plume dimensions
AIAA | 1969
|Rocket exhaust plume phenomenology
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|PNS simulation of rocket exhaust nozzle flows
AIAA | 1988
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