Paper summarizes for first time methods used for estimation of critical Mach number on bodies, wings and tail units; it is shown that value of merit depends not only on magnitude of supervelocity but also on its direction and on direction of isobars. (see also - n 2042 July 28 1950 p 110-3)


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    Titel :

    Estimation of critical Mach number


    Weitere Titelangaben:

    Aeroplane


    Beteiligte:
    Lee, G.H. (Autor:in)

    Erschienen in:

    Aeroplane ; 79 , n 2046


    Erscheinungsdatum :

    1950


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Form Factor and Critical Mach Number Estimation for Finite Wings

    Takahashi, Timothy J. / German, Brian J. / Shajanian, Arvin et al. | AIAA | 2012



    Rotorcraft Airfoil Performance Near Critical Mach Number

    Bonilla, C. / Gompertz, K. / Thake, M. et al. | British Library Conference Proceedings | 2012


    Critical Mach Number Prediction on Swept Wings

    Kirkman, Jeffrey J. / Takahashi, Timothy T. | AIAA | 2017


    Rotorcraft Airfoil Performance Near Critical Mach Number

    Bonilla, Carlos / Gompertz, Kyle / Thake, Michael et al. | AIAA | 2012