New method of calculation makes direct use of actual airplane polars without approximations; procedure based on extension of Eiffel-Rith coordinate system, and all scales can be incorporated in simple transparent chart, thereby eliminating necessity for special prepared graph paper; compressibility effects are taken into account through use of constant altitude variable Mach number polars which are derived from constant Mach number polars of true airplane. (see also J Aeronautical Sciences v 11 n 4 Oct 1944 p 329-38)


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    Titel :

    Logarithmic performance computation


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Foa, J.V. (Autor:in) / Leadon, B.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1944


    Anmerkungen:

    Bibliography


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Logarithmic performance computation

    Foa, J.V. / Leadon, B.M. | Engineering Index Backfile | 1944





    Thermal performance of a logarithmic-spiral resonance tube

    NEEMEH, R. A. / OSTROWSKI, P. P. / WU, J. H. T. | AIAA | 1984