Determining exit conditions that result when heat is withdrawn from rocket thrust chamber and added to gas flow in nozzle


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    Title :

    Effect of chamber-to-nozzle heat exchange on frozen and equilibrium flows in De Laval nozzles


    Contributors:

    Publication date :

    1970-04-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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