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    Title :

    CONJUGATE HEAT TRANSFER SIMULATION OF A SUBSCALE ROCKET THRUST CHAMBER USING A TIMESCALE BASED FROZEN NON-ADIABATIC FLAMELET COMBUSTION MODEL


    Contributors:

    Conference:

    AIAA Propulsion and Energy Forum ; 2019 ; Indianapolis, Ind.



    Publication date :

    2019



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    55.50 Luftfahrzeugtechnik / 58.21 Brennstoffe, Kraftstoffe, Explosivstoffe / 55.60 Raumfahrttechnik






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