Abstract
Boundary Layers, Journal of Aircraft, Vol. 7, No. 2, March-April 1970, pp. 137-140. Schlichting, H., Boundary Layer Theory, 6th ed., McGrawHill, New York, 1968, p. 555. Van Driest, E. R., Boundary Layer in Compressible Fluids, Journal of the Aeronautical Sciences, Vol. 18, 1951, pp. 145-160, 216. Maise, G. and McDonald, H., Mixing Length and Kinematic Eddy Viscosity in a Compressible Boundary Layer, AIAA Journal, Vol. 6, No. 1, Jan. 1968, pp. 73-80. Klebanoff, P., Characteristics of Turbulence in a Boundary Layer with Zero Pressure Gradient, TN 3178,1954, NACA. Horstman, C. and Owen, F., Properties of a Compressible Boundary Layer, AIAA Journal, Vol. 10, No. 11, Nov. 1972, pp. 1418-1424. Seebaugh, W., An Investigation of the Interaction of a Shock Wave and a Turbulent Boundary Layer in Axially-Symmetric Internal Flow Including the Effect of Mass Bleed, Ph.D. thesis, 1968, Univ. of Washington, Seattle, Wash. Teeter, G., An Experimental Investigation of the Interaction of a Shock Wave with a Decelerated Turbulent Boundary Layer, M.S. thesis, 1971, Univ. of Washington, Seattle, Wash. Rose, W., The Behavior of a Compressible Turbulent Boundary Layer in a Shock-Wave-Induced Adverse Pressure Gradient, Ph.D. thesis, 1972, Univ. of Washington, Seattle, Wash.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.