Buffet onset measurements on an Aircraft model at transonic mach numbers

Viswanath, PR (1986) Buffet onset measurements on an Aircraft model at transonic mach numbers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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    Abstract

    Buffet onset measurements have been performed on a low13; aspect ratio, moderately swept, aircraft model at three13; transonic Mach numbers in the 1.2m tunnel. Instrumentation13; included wing root strain gauges, a wing tip accelerometer13; wing trailing edge pressure taps and standard six component13; internal obtained strain gauge balance. Results of buffet onset 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.

    Item Type: Proj.Doc/Technical Report (Technical Report)
    Uncontrolled Keywords: Buffet onset;Buffet response;Transonic buffet
    Subjects: AERONAUTICS > Aerodynamics
    Division/Department: Aerodynamics
    Depositing User: M/S ICAST NAL
    Date Deposited: 04 Sep 2006
    Last Modified: 24 May 2010 09:50
    URI: http://nal-ir.nal.res.in/id/eprint/2617

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