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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    Titel :

    Combustion in liquid-fuel rocket


    Weitere Titelangaben:

    Aeronautical Quarterly


    Beteiligte:
    Spalding, D.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    27 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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