Abstract

References *Mack, L. M., Stability Theory and the Problem of Supersonic Boundary-Layer Transition, AIAA Journal, Vol. 13, No. 3, 1975, pp. 278-298. Mack, L. M., Layer Linear Stability Theory, AGARD Kept. 709, June 1984. Potter, J. L., Review of the Influence of Cooled Walls on Boundary Layer Transition, AIAA Journal, Vol. 18, No. 1980, pp. 1010-1012. Sanator, R. J., DeCarlo, J. P., and Torrillo, D. T., Boundary Layer Transition Data for a Cold-Wall Slender Cone, AIAA Journal, Vol. 3, No. 4, 1965, pp. 758-760. Stetson, K. F., and Rushton, G. H., Shock Tunnel Investigation of Boundary Layer Transition at M = 5.5, AIAA Journal, Vol. 5, No. 5, 1967, pp. 899-906. Mateer, G. G., Effects of Wall Cooling and Angle of Attack on Boundary-Layer Transition on Sharp Cones at Moo = 7.4, NASA TD D-6908, Aug. 1972. Stetson, K. F., Kimmel, R. L., Thompson, E. R., Donaldson, J. C., and Siler, L. G., A Comparison of Planar and Conical Boundary Layer Stability and Transition at a Mach Number of 8, AIAA Paper 91-1639, June 1991. Kendall, J. M., Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary Layer Transition, AIAA Journal, Vol. 13, No. 3, 1975, pp. 290-299. Demetriades, A., New Experiments on Hypersonic Boundary Layer Stability Including Wall Temperature Effects, Proceedings of the Heat Transfer and Fluid Mechanics Institute, edited by C. T. Crowe and W. L. Grosshandler, Stanford Univ. Press, Stanford, CA, 1978, pp. 39-54.

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