Abstract
21 Winkler, E. M., Design and calibration of stagnation temperature probes for use at high supersonic speeds and elevated temperature, J. Appl. Phys. 25, 231-232 (February 1954). 22 Danberg, J. E., The equilibrium temperature probe, a device for measuring temperatures in hypersonic boundary layers/' U. S. Naval Ordnance Lab., White Oak Md., NOL TR 61-2 (February 1962). 23 Hill, F. K., Turbulent boundary layer measurements at Mach numbers from 8 to 10, Phys. Fluids 2, 668-680 (1959). 24 Bertram, M. H. and Neal, L., Jr., Recent experiments in hypersonic turbulent boundary layers, NASA Langley Research Center, Langley Station, Va.; also presented at AGARD Specialist Meeting on Recent Development in Boundary Layer Research, Naples, Italy (May 1965). 25 Cohen, N. B., A method for computing turbulent heat transfer in the presence of a streamwise pressure gradient for bodies in high-speed flow, NASA Memo. 1-2-59L (March 1959). 26 Walz, A., Compressible turbulent boundary layers, International Symposium on the Mechanique de le Turbulence (Centre National de la Recherche Scientifique, Paris, 1962), pp. 299-350. 27 McLafferty, G. H. and Barrer, R. E., The effect of adverse pressure gradients on the characteristics of turbulent boundary layers in supersonic stream, J. Aerospace Sci. 29, 1-10(1962). 28 Kepler, C. E. and O'Brien, R. L., Supersonic turbulent boundary layer growth over cooled walls in adverse pressure gradients, United Aircraft Corp., Aeronautical Systems Div. ASD-TDR-62-87 (October 1962). 29 Burke, A. F., Turbulent boundary layers on highly cooled surfaces at high Mach numbers, Proceedings of Symposium on Aerothermoelasticity, Dayton, Ohio (1961), pp. 704-741; also U.S. Air Force, Aeronautical Systems Div., Wright-Patterson Air Force Base, Ohio, TR 6-645 (1961). 30 Morkovin, M. V., Effects of high acceleration on a turbulent supersonic shear layer, Proceeding of the 1955 Heat Transfer and Fluid Mechanics Institute (Stanford University Press, Stanford, Calif., 1955), pp. IV, I-IV, 17. 31 Libby, P. A. and Baronti, P. O., A transformation theory of the turbulent compressible boundary layer with pressure gradient and heat transfer, General Applied Science Labs., Inc., TR 455 (August 1964).
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