Buffet onset measurements were performed on a low aspect ratio, moderately swept, aircraft model at three transonic Mach numbers in the 1.2 m tunnel. Instrumentation included wing root strain gauges, a wing tip accelerometer, wing trailing edge pressure taps, and standard six component internal strain gauge balance. Results of buffet onset obtained by these different techniques are compared. A discussion of the buffet onset results, as it relates to the main features of the flow on the wing upper surface, is also included.


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    Titel :

    Buffet Onset Measurements on an Aircraft Model at Transonic Mach Numbers


    Beteiligte:

    Erscheinungsdatum :

    1986


    Format / Umfang :

    39 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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