Wall Shear at a Three-Dimensional Stagnation Point with a Moving Wall

Abstract

1 Lees, L. and Reeves, B. L., Supersonic Separated and Reattaching Laminar Flows: 1 General Theory and Application to Adiabatic Boundary Layer/Shock Wave Interactions, AIAA Journal, Vol. 2, No. 11, Nov. 1964, pp. 1907-1920. 2 Gautier, B. G. and Ginoux, J. J., A Theoretical Study of Wall Cooling Effects upon Shock Wave-Laminar Boundary Layer Interaction by the Method of Lees-Reeves-Klineberg, TN 71, May 1971, von Karman Institute, Rhode-St-Genese, Belgium. 3 Stewartson, K., Further Solutions of the Falkner-Skan Equation, Proceedings of the Cambridge Philosophical Society, Vol. 50, 1954, pp. 454-465. 4 Rogers, D. F., Reverse Flow Solutions for Compressible Laminar Boundary-Layer Equations, The Physics of Fluids, Vol. 12, No. 3, March 1969, pp. 527-533. 5 Keller, H. B. and Cebeci, T., An Inverse Problem in BoundaryLayer Flows: Numerical Determination of Pressure Gradient for a Given Wall Shear, Journal of Computational Physics, Vol. 10, No. 1, Aug. 1972, pp. 151-161. 6 Libby, P. A. and Liu, T. M., Some Similar Laminar Flows Obtained by Quasilinearization, AIAA Journal, Vol. 6, No. 8, Aug. 1968, pp. 1541-1548. 7 Wortman, A. and Mills, A. F., Separating Self-Similar Laminar Boundary Layers, AIAA Journal, Vol. 9, No. 12, Dec. 1971, pp. 2449-2451. Table 1 Wall values for several values of the parameter c