A numerical analysis on three-dimensional flow field in a supersonic bump-type inlet

Author:

Kim Sang Dug,Song Dong Joo

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Reference13 articles.

1. Anderson, J., 1990, “Airframe/Propulsion Integration of Supersonic Vehicles,” 26th AIAA/ SAE/ASME/ASEE Joint Proportion Conference, AIAA 90–2151, Orlando, Fl, July.

2. Benson, J. and Miller, L. D., 1991, “Mach 5 Turbo-Ramjet Inlet Design and Performance,” ISABE 91–7079, ISABE Conference, Nottingham, U.K., September, Vol. 12, pp. 746–753.

3. Gridley, M. C. and Walker, S. H. 1996,Advanced Aero-Engine Concepts and Controls, AGARD Conf. Proc. 572, 86th Symposium, Seattle, WA.

4. Hirsh, C., 1989,Numerical Computation of Internal and External Flows, Vol. 2 JOHN WILEY & SONS, NY, pp. 493–594.

5. Kim, S. D., Kwon, C. O. and Song, D. J., 2004, “Comparison of Turbulence Models in Shock-Wave/Boundary-Layer Interaction,”KSME International Journal, Vol. 18, No. 1, pp. 153–166.

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