On the Non-Uniqueness of the Parallel-Flow Approximation
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Publisher
Springer New York
Link
http://link.springer.com/content/pdf/10.1007/978-1-4612-2956-8_34.pdf
Reference11 articles.
1. Balakumar, P., and M. R. Malik, 1991 “Waves produced from a harmonic point source in a supersonic boundary layer,” AIAA Paper No. 91-1646.
2. Duck, P. W., and S. J. Shaw, 1990 “The inviscid stability of supersonic flow past a sharp cone”, ICASE Report No. 90-14.
3. El-Hady, N. M., 1991 “Nonparallel instability of supersonic and hypersonic boundary layers,” AIAA Paper No. 91-1324.
4. Erlebacher, G., and M. Y. Hussaini, 1990 “Numerical experiments in supersonic boundary-layer stability,” Phys. Fluids A, Vol. 2, No. 1, pp. 94–104.
5. Gasperas, G., 1987 “The stability of the compressible boundary layer on a sharp cone at zero angle of attack,” AIAA Paper No. 87-0494.
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1. Spatial direct numerical simulation of high-speed boundary-layer flows Part II: Transition on a cone in Mach 8 flow;Theoretical and Computational Fluid Dynamics;1995-09
2. Modeling of nonparallel effects in temporal direct numerical simulations of compressible boundary-layer transition;Theoretical and Computational Fluid Dynamics;1995-02
3. On the accurate prediction of the wall-normal velocity in compressible boundary-layer flow;International Journal for Numerical Methods in Fluids;1993-01-30
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