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  • 1
    Publication Date: 2019-06-28
    Description: Calculations were made of the effects of surface waviness on the external pressure of a supercritical airfoil at design conditions. Wave parameters varied include amplitude, wavelength, phase, and number of cycles. Effects of single and multiple waves are calculated at various chordwise locations. General trends of surface waviness effects on pressure distribution are determined and these solutions are reported. Contour deviations are imposed on the upper surface of the airfoil. Results are presented in a manner designed to facilitate ready comparison with the ideal contour static pressure distribution.
    Keywords: AERODYNAMICS
    Type: NASA-TM-85705 , NAS 1.15:85705
    Format: application/pdf
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