The variation of the intensity of buffeting experienced throughout the operational region of the semitailless Northrop X-4 airplane and the values of maximum and peak normal-force coefficients in the Mach number range from 0.42 to 0.92 have been determined. The results are compared with data obtained with the swept-wing Douglas D-558-II airplane.


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    Titel :

    Results of Measurements of Maximum Lift and Buffeting Intensities Obtained During Flight Investigation of the Northrop X-4 Research Airplane


    Beteiligte:

    Erscheinungsdatum :

    20.08.1953


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch