Heat transfer coefficients in rocket nozzle cooling passages predicted by equation developed from hydrogen flow experiments


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    Title :

    Heat-transfer predictions in the cooling passages of nuclear rocket nozzles.


    Contributors:

    Conference:

    PROPULSION JOINT SPECIALIST CONFERENCE ; 1968 ; CLEVELAND, OH


    Publication date :

    1968-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English