Abstract

3 Dernetriades, A., An Investigation of the Stability of the Laminar Layer, Memo 43, 1958, Guggenheim Aeronautical Lab., California Institute of Technology. 4 Potter, J. L. and Whitfield, J. D., Effects of Unit Reynolds Number, Nose Bluntness, and Roughness on Layer Transition, TR-60-5, 1960, Arnold Engineering Development Center. 5 Nagamatsu, H. T., Graber, B. C., and Sheer, R. E., Jr., Critical Layer Concept Relative to Layer Stability/' Rept. 66-C-192, 1966, General Electric Co. 6 Maddalon, D. V. and Henderson, A., Jr., Transition on Sharp Cones at Mach Numbers, AIAA Journal, Vol. 6, No. 3, March 1968, pp. 424-431. 7 Softley, E. J. and Graber, B. C., Experimental Observation of Transition of the Layer, AIAA Journal, Vol. 7, No. 2, Feb. 1969, pp. 257-263. 8 Deem, R. E. and Murphy, J. S., Flat Plate Layer Transition at Speeds, AIAA Paper 65-128, New York, 1965. 9 Sanator, R. J., DeCarlo, J. P., and Torrillo, D. T., Hypersonic Boundary-Layer Transition Data for a Cold-Wall Slender Cone, AIAA Journal, Vol. 3, No. 4, April 1965, pp. 758-760. 10 Rouse, H., A General Stability Index for Flow Near Plane Boundaries, Journal of the Aeronautical Sciences, Vol. 12, No. 4, Oct. 1945, pp. 429-431. 11 Rouse, H., Elementary Mechanics of Fluids, Wiley, New York, 1946, p. 172. 12 Cohen, N. B., Boundary Layer Similar Solutions and Correlation Equations for Laminar Heat-Transfer Distributions in Equilibrium Air at Velocities up to 41,000 Feet Per Second, TR R-118,1961, NASA. 13 van Driest, D. R. and Blumer, C. B., Boundary Layer Transition: Freestream Turbulence and Pressure Gradient Effects, AIAA Journal, Vol. 1, No. 6, June 1963, pp. 1303-1306. 14 Iverson, H. W. and Hsu, T.-T., A Local Reynolds Number to Predict Transition from Laminar to Turbulent Flow, Heat Transfer Thermodynamics and Education, McGraw-Hill, New York, pp. 207-212. BOUNDARY LAYER

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