Droplet vaporization, chemical reaction, and drag between gas and droplet are considered for 1-dimensional model; quantitative theoretical results are presented for variation of droplet size, droplet velocity, gas temperature and gas velocity within chamber, particular attention being paid to calculation of specified ratio therefor; theory applied to German V2 rocket motor.


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    Title :

    Combustion in liquid-fuel rocket


    Additional title:

    Aeronautical Quarterly


    Contributors:

    Published in:

    Publication date :

    1959


    Size :

    27 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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