A new shock tunnel facility for high compressibility mixing layer studies
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[1] Nagi N. Mansour,et al. The structure of the compressible reacting mixing layer: Insights from linear stability analysis , 1998 .
[2] T. Island. Quantitative scalar measurements and mixing enhancement in compressible shear layers , 1997 .
[3] M. Mungal,et al. Small-perturbation mixing enhancement in compressible shear layers , 1997 .
[4] Noel T. Clemens,et al. Large-scale structure and entrainment in the supersonic mixing layer , 1995, Journal of Fluid Mechanics.
[5] Dimitri Papamoschou,et al. Evidence of shocklets in a counterflow supersonic shear layer , 1995 .
[6] A. Majda,et al. Singular front formation in a model for quasigeostrophic flow , 1994 .
[7] J. Ferziger,et al. Linear stability of the compressible reacting mixing layer , 1993 .
[8] Parviz Moin,et al. EDDY SHOCKLETS IN DECAYING COMPRESSIBLE TURBULENCE , 1991 .
[9] Neil D. Sandham,et al. Three-dimensional simulations of large eddies in the compressible mixing layer , 1991, Journal of Fluid Mechanics.
[10] Paul E. Dimotakis,et al. Experiments in nonreacting compressible shear layers , 1991 .
[11] Mo Samimy,et al. Effects of compressibility on the characteristics of free shear layers , 1990 .
[12] Otto Zeman,et al. Dilatation dissipation: The concept and application in modeling compressible mixing layers , 1990 .
[13] Thomas L. Jackson,et al. Inviscid spatial stability of a compressible mixing layer , 1989, Journal of Fluid Mechanics.
[14] A. Roshko,et al. The compressible turbulent shear layer: an experimental study , 1988, Journal of Fluid Mechanics.
[15] Goro Masuya,et al. Spreading of two-stream supersonic turbulent mixing layers , 1986 .
[16] D. W. Bogdanoff,et al. Compressibility Effects in Turbulent Shear Layers , 1983 .
[17] G. E. Chmielewski,et al. Boundary-Layer Considerations in the Design of Aerodynamic Contractions , 1974 .
[18] R. Wagner. Mean flow and turbulence measurements in a Mach 5 free shear layer , 1973 .
[19] M. Dunn. Experimental study of high-enthalpy shock- tunnel flow. I - Shock-tube flow and nozzle starting time. , 1969 .
[20] J. A. Fox,et al. Stability of the laminar mixing of two parallel streams with respect to supersonic disturbances , 1966, Journal of Fluid Mechanics.
[21] W. S. King,et al. Series solutions for shock tube laminar boundary layer and test time. , 1966 .
[22] Harold Mirels,et al. TEST TIME IN LOW PRESSURE SHOCK TUBES , 1963 .
[23] D. White,et al. Flow in shock tubes with area change at the diaphragm section , 1958, Journal of Fluid Mechanics.