Hostname: page-component-7479d7b7d-t6hkb Total loading time: 0 Render date: 2024-07-12T04:26:39.328Z Has data issue: false hasContentIssue false

An experimental study of turbulent separating and reattaching flows at a high Mach number

Published online by Cambridge University Press:  29 March 2006

J. P. Batham
Affiliation:
Central Electricity Research Laboratories, Leatherhead

Abstract

Separating and reattaching flows in a two-dimensional compression corner were investigated experimentally at a Mach number of 7·0 and Reynolds numbers (based on the distance from the leading edge to the corner) of 4·75 × 106, 9·51 × 106 and 1·55 × 107. Heat-transfer measurements and Pitot traverses in the upstream boundary layer showed that the boundary layer had become fully turbulent at the start of the interactions. Increases in the Reynolds number gave increases in the length of separated shear layers and decreases in the corner angle required for incipient, separation. The reattachment pressure coefficients gave good agreement with the criterion of Batham (1969).

Type
Research Article
Copyright
© 1972 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Batham, J. P. 1969 A.I.A.A. J. 7, 154.
Bushnell, D. M., Johnson, C. B., Harvey, W. D. & Fellor, W. V. 1969 N.A.S.A. Tech. Note, no. D-5433.
Coleman, O. T., Elxstrom, G. M. & Stollery, J. L. 1971 AGARD Cmf. Preprint, no. 93.
Danberq, J. E. 1964 Nov. Org. Lab. Tech. Rep. no. 64–99.
Drotjgge, G. 1953 P.F.A. Sweden Rep. no. 46.
East, R. A. & Perry, J. H. 1967 Aero. Res. Counc. Current Paper, no. 909.
Erdos, J. & Pallone, A. 1962 Proc. 1962 Heat Transfer and Fluid Mechanics Inst.
Holloway, P. F., Sterrett, J. R. & Creekmore, H. S. 1965 N.A.S.A. Tech. Note, no. D-3074.
Hopkins, E. J., Rubesin, M. W., Inouye, M., Keener, E. R., Mateer, G. C. & Polek, T. E. 1969 N.A.S.A. Tech. Note, no. D-5089.
Kuehn, D. M. 1959 N.A.S.A. Memo. no. 1-21-59 W.
La Graff, J. E. 1969 Dept. of Eng. Sci., Oxford University. Rep. no. 109469.
La Graff, J. E., Batham, J. P. & Owen, F. K. 1969 Aero. Res. Counc. 31, 246 Hyp. 757.
Lewis, J. E., Kubota, T. & Lees, L. 1968 A.I.A.A. J. 6, 7.
Meyer, R. F. 1963 Nat. heron. Establishment of Canada Rep. no. LR-375.
Roshko, A. & Thomke, G. J. 1969 Proc. Symposium on Viscous Interaction Phenomena in Supersonic and Hypersonic Flow. U.S.A.F. A.R.L., Ohio.
Sterrett, J. R. & Emery, J. C. 1962 N.A.S.A. Tech. Note, no. D-1014.
Walz, A. 1961 Proc. Symposium on the Mechanics of Turbulence, C.R.N.S. Marseille.