The Shock-Wave/Turbulent Boundary-Layer Interaction on Curved Surface at Transonic Speed

Author:

Liu X.,Squire L. C.

Publisher

Springer Berlin Heidelberg

Reference7 articles.

1. Baker C.J. (1980) The prediction of boundary layer development through a normal shock wave turbulent boundary-layer interaction, Cambridge University, CUED/A-AERO/TR.10 (1980)

2. Bryanston-Cross P.J. and Denton J. D. (1982) Comparison of interferometric measurements and computed flow around a wedge profile in the transonic region, ASME paper 82-GT-258

3. Denton J.D. (1983) An improved time-marching method for turbomachinery flow calculation, Transactions of the ASME, Journal of Engineering for power, Vol. 105, July 1983, pp514-521

4. Green J.E., Weeks D.J. and Brooman J.W.F. (1972) Prediction of turbulent boundary layers and wakes in compressible flow by a lag-entrainment method, R.A.E. T.R.72231

5. Inger G.R. and Mason W.H. (1976) Analytical theory of transonic normal shock-turbulent boundary-layer interaction, AIAA J. vol.14, No.9, p.1266

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