Fluctuating wall pressures near separation in highly swept turbulent interactions

Fluctuating wall pressures have been measured in Mach 5 interactions generated by sharp, upswept fins at angles of attack of 16 to 28 deg. The results show that rms pressure distributions, like the mean, can be collapsed in conical coordinates. The wall pressure signal near separation is intermittent and is qualitatively similar to that measured in unswept interactions and other swept flows. However, the dominant separation shock frequencies in the swept flows are up to an order of magnitude higher than those in unswept interactions under identical incoming flow conditions. In light of the present observations, it appears that an earlier remark, by Gilson and Dolling, that separation is characterized by a shuddering compression system, in contrast to a translating separation shock is erroneous due to a combination of weak shock strength and inadequate spatial resolution. Furthermore, although the maximum rms pressure near separation increases with increasing interaction strength, as in swept compression ramp flows, comparison of data from the two flow types indicates that the appropriate correlating parameter is the interaction sweepback angle.

[1]  G. Settles,et al.  Structure of swept shock wave/boundary-layer interactions using conical shadowgraphy , 1990 .

[2]  D. Dolling,et al.  Exploratory study of wall pressure fluctuations in a Mach 5, sharp fin-induced turbulent interaction , 1992 .

[3]  G. Settles,et al.  Wall pressure fluctuations beneath swept shock wave/boundary layer interactions , 1993 .

[4]  D. Dolling,et al.  Correlation of interaction sweepback effects on unsteady shock-induced turbulent separation , 1993 .

[5]  D. Dolling,et al.  Effects of Sweepback on Unsteady Separation in Mach 5 Compression Ramp Interactions , 1993 .

[6]  Gary S. Settles,et al.  Swept shock/boundary-layer interactions - Tutorial and update , 1990 .

[7]  Farrukh S. Alvi,et al.  Physical Model of the Swept Shock Wave/Boundary-Layer Interaction Flowfield , 1992 .

[8]  Wall pressure fluctuations near separation in a Mach 5, sharp fin-induced turbulent interaction , 1991 .

[9]  D. Knight,et al.  On the quasi-conical flowfield structure of the swept shock wave-turbulent boundary layer interaction , 1991 .

[10]  D. Tan,et al.  Surface pressure fluctuations in a three-dimensional shock wave/turbulent boundary layer interaction at various shock strengths , 1985 .

[11]  D. Tan,et al.  Wall pressure fluctuations in a three-dimensional shock-wave/turbulent boundary interaction , 1987 .

[12]  G. Settles,et al.  Inception length to a fully-developed fin-generated shock wave boundary-layer interaction , 1989 .

[13]  Gary S. Settles,et al.  Flow visualization methods for separated three-dimensional shock wave/turbulent boundary-layer interactions , 1983 .

[14]  J. Schmisseur,et al.  Unsteady separation in sharp fin-induced shock wave/turbulent boundary layer interaction at Mach 5 , 1992 .

[15]  G. Settles,et al.  Mach number effects on conical surface features of swept shock-wave/boundary-layer interactions , 1987 .

[16]  D. Dolling,et al.  Computation of turbulent, separated, unswept compression ramp interactions , 1992 .