Turbulence Measurements in a Compressible Reattaching Shear Layer

Detailed hot-wire measurements of the longitudinal component of the mass-flow fluctuations have been made in an approximately self-preserving free shear layer reattaching on a 20-deg ramp at Mach number 2.9. The experimental configuration is especially designed to provide a well-defined initial condition for the reattachment process. The absolute mass-flow turbulence intensity increases dramatically through the compression in the reattachment region, which is in sharp contrast to similar subsonic reattachments. It is clear that the mean dilatation contributes significantly to the turbulence amplification. In addition, the length scale is affected strongly by the presence of extra strain rates. Prediction of this flow will require some sophisticated modeling, and the challenge to the predictor is clear.

[1]  Alexander J. Smits,et al.  The effect of short regions of high surface curvature on turbulent boundary layers , 1978, Journal of Fluid Mechanics.

[2]  I. Wygnanski,et al.  The two-dimensional mixing region , 1970, Journal of Fluid Mechanics.

[3]  Hot-wire investigation of an unseparated shock-wave/turbulent boundary-layer interaction , 1984 .

[4]  P. Bradshaw The effect of mean compression or dilatation on the turbulence structure of supersonic boundary layers , 1974, Journal of Fluid Mechanics.

[5]  Gary S. Settles,et al.  A Reattaching Free Shear Layer in Compressible Turbulent Flow: A Comparison of Numerical and Experimental Results , 1981 .

[6]  Peter Bradshaw,et al.  Calculation of boundary-layer development using the turbulent energy equation: compressible flow on adiabatic walls , 1971, Journal of Fluid Mechanics.

[7]  Gary S. Settles,et al.  Reattachment of a Compressible Turbulent Free Shear Layer , 1982 .

[8]  A. Smits A visual study of a separation bubble. , 1982 .

[9]  P. Bradshaw Effects of Streamline Curvature on Turbulent Flow. , 1973 .

[10]  Gary S. Settles,et al.  A study of reattachment of a free shear layer in compressible turbulent flow , 1980 .

[11]  D. M. Bushnell,et al.  Numerical computations of turbulence amplification in shock wave interactions , 1984 .

[12]  A. Smits,et al.  Constant temperature hot-wire anemometer practice in supersonic flows , 1983 .

[13]  P. Bradshaw Calculation of boundary-layer development using the turbulent energy equation , 1967, Journal of Fluid Mechanics.

[14]  Peter Bradshaw,et al.  Turbulence structure of a reattaching mixing layer , 1981, Journal of Fluid Mechanics.

[15]  A. Smits,et al.  The response of a turbulent boundary layer to lateral divergence , 1978, Journal of Fluid Mechanics.

[16]  L. Kovasznay,et al.  The Hot-Wire Anemometer in Supersonic Flow , 1950 .

[17]  P. Bradshaw,et al.  The reattachment and relaxation of a turbulent shear layer , 1972, Journal of Fluid Mechanics.

[18]  J. C. Anyiwo,et al.  Turbulence amplification in shock-wave boundary-layer interaction , 1982 .