Abrupt and gradual stalls were made in Mach ranges of 0.21-0.63 and 0.41-0.65 respectively. Abrupt pull-ups were made through Mach range of 0.21- 0.30. Mach number greatly affected maximum lift coefficient and buffeting boundary line. Buffeting boundary was defined by maximum lift coefficient only up to M = 0.64. Above M = 0.12, calculations lost their agreement with flight data. Gradual stalls showed same effect of Mach number as abrupt stalls.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Effect of Mach Number on the Maximum Lift and Buffeting Boundary Determined in Flight on a North American P-51D Airplane


    Beteiligte:
    J. P. Mayer (Autor:in)

    Erscheinungsdatum :

    1947


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch