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    A study of flow separation on an aspect ratio three flap at Mach number 2.4 (1991)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: Static pressure distributions and dark central ground interferometry are used to document the flow on a flap over a range of Reynolds numbers and deflection angles. The pressure profiles and interferograms are analyzed to distinguish laminar, transitional and turbulent flows in attached, incipient and separated cases. Sideplates are used to compare two and three dimensional effects. Data is also presented for extended flaps used to isolate the effect of the trailing edge expansion. The issues of unsteadiness and hysteresis are also addressed.
    Keywords: AERODYNAMICS
    Type: AIAA PAPER 91-1620
    Format: text
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