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.


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    Titel :

    Chemical Kinetic/Gas Dynamic/Particle Interactions in Rocket Nozzle and Exhaust Plume Flows


    Beteiligte:
    H. S. Pergament (Autor:in) / R. D. Thorpe (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Problems of rocket exhaust plume interactions.

    Dattorre, L. / Yoshihara, H. | NTRS | 1968


    Rocket exhaust plume dimensions

    DYNER, H. B. | AIAA | 1969


    JANNAF handbook rocket exhaust plume technology / Chemical Propulsion Information Agency; [JANNAF Exhaust Plume Technology Subcommittee] ; Chapter 3: Rocket exhaust plume radiation

    Chemical Propulsion Information Agency / USA, Joint Army Navy NASA Air Force Exhaust Plume Technology Subcommittee | TIBKAT | 1980


    Rocket exhaust plume phenomenology

    Simmons, Frederick S. | TIBKAT | 2000