Two complementary approaches are being followed at NASA Lewis Research Center; attempt is made to devise simplified conceptual models of combustion system that give quantitative predictions of system behavior from conservation equations; predictions must be checked experimentally; individual rate processes are studied to attain more realistic models; example of each approach to learning is given.


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    Titel :

    Recent aspects of rocket combustion research


    Weitere Titelangaben:

    NASA -- Proc


    Beteiligte:
    Morrell, G. (Autor:in) / Priem, R.J. (Autor:in)

    Kongress:

    NASA -- University Conference on Science and Technology of Space Exploration ; 1962 Combustion


    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aspects of combustion stability in liquid propellant rocket motors

    Crocco, L. | Engineering Index Backfile | 1952


    Aspects of combustion stability in liquid propellant rocket motors

    Crocco, L. | Engineering Index Backfile | 1951



    Supersonic-Combustion Rocket

    R. J. Weber / L. C. Franciscus | NTIS | 1973