Abstract
with emphasis on the structure of the jet and separation ahead of the jet, Separated Flow, Part 2, Proceedings of a Specialists Meeting, AGARD Fluid Dynamics Panel (AGARD, Paris, France 1966), pp. 667-700. 16 Needham, D. A. and Stallery, J. L., Boundary layer separation in-hypersonic flow, AIAA Paper 66-455 (1966). 17 Maurer, F., Interaction effects of lateral control jets expanding into a supersonic flow, Deutsche Versuchsanstalt fur Luftund Raumfahrt, Munich, Germany Rept. 65-04 (1965). 18 Wu, J.-M., personal communication, based on R. E. Wilson, An experimental investigation of separated turbulent supersonic flow at M = 3.0, M.S. Thesis, Univ. of Tennessee (June 5, 1966). 19 Reshotko, E. and Tucker, M., Effect of a discontinuity on turbulent boundary-layer-thickness parameters with application to shock-induced separation, NACA TN 3454 (May 1955). 20 Mager, A., On the model of the free shock-separated turbulent boundary layer, J. Aeronaut. Sci. 23, 181-184 (1956). 21 Zukoski, E. E., Review of data concerning turbulent boundary layer separation in front of a forward facing step, Guggenheim Jet Propulsion Center, California Institute of Technology, Pasadena, Calif., Rept. 66-8-15-1 (August 1966).
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