Stability of Compressible Boundary Layers

作者: W. BYRON BROWN

DOI: 10.2514/3.4300

关键词:

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

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