Experimental procedure developed to measure gas film heat transfer coefficients in rocket motor combustion chambers and nozzles; procedure utilizes transient temperature rise of uncooled segmented walls of rocket motor to determine rate of heat transfer.


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    Title :

    Determination of rocket-motor heat-transfer coefficients by transient method


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1951


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English