Calculations of steady-state temperatures, and of temperature, mass, and trajectory histories of droplets in h-p and high-temperature environments were made to determine under what conditions critical point is reached by vaporizing drops; liquid heptane and liquid oxygen propellants were studied; boundary conditions for calculations were representative of those occurring in high-intensity combustion fields that exist in rocket engines; total gas pressures up to 2000 psi were investigated; results are presented graphically; significance to combustor design and to combustion-instability mechanisms is shown.


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    Titel :

    Calculated temperature histories of vaporizing droplets to critical point


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Wieber, P.R. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 12 ; p 2764-2770


    Erscheinungsdatum :

    1963


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Experimental and calculated histories of vaporizing fuel drops

    Priem, R J / Borman, G L / El Wakil, M M et al. | NTRS | 1957



    Experimental and calculated temperature and mass histories of vaporizing fuel drops

    El Wakil, M.M. / Priem, R.J. / Brikowski, H.J. et al. | Engineering Index Backfile | 1956