Linearized theory is applied to determine lift coefficient and efficiency of heat addition and to optimize wing profile, angle of attack, and heat addition; comparison with conventional ramjet and wing shows ramjet to be superior on range basis up to Mach number of about 8. (Derivation of Effect of Supersonic Underwing Heat Addition from Potential-Flow Equations)


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    Titel :

    Analysis and evaluation of supersonic underwing heat addition


    Weitere Titelangaben:

    NASA -- Memo


    Beteiligte:
    Luidens, R.W. (Autor:in) / Flaherty, R.J. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    55 pages


    Anmerkungen:

    Appendix C


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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