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    Turbulent Boundary Layer on a Yawed Cone in a Supersonic Stream (1959)
    In:  CASI
    Details
    Publication Date: 2019-08-16
    Description: The momentum integral equations are derived for the boundary layer on an arbitrary curved surface, using a streamline coordinate system. Computations of the turbulent boundary layer on a slightly yawed cone are made for a Prandtl number of 0.729, wall to free-stream temperature ratios of 1/2, 1, and 2, and Mach numbers from 1 to 4. Deflection of the fluid in the boundary layer from outer stream direction, local friction coefficient, displacement surface, lift coefficient, and pitching-moment coefficient are presented.
    Keywords: Fluid Mechanics and Heat Transfer
    Type: NASA-TR-R-7
    Format: application/pdf
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