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    Effect of Surface Waviness on Transition in Three-Dimensional Boundary-Layer Flow (1996)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The effect of a surface wave on transition in three-dimensional boundary-layer flow over an infinite swept wing was studied. The mean flow computed using interacting boundary-layer theory, and transition was predicted using linear stability theory coupled with the empirical eN method. It was found that decreasing the wave height, sweep angle, or freestream unit Reynolds number, and increasing the freestream Mach number or suction level all stabilized the flow and moved transition onset to downstream locations.
    Keywords: Aerodynamics
    Type: NASA-CR-201641 , NAS 1.26:201641
    Format: application/pdf
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