Original Article
2005, Young, D., Jenkins, S. and Miller, D., “An investigation of active flowfield control for inlet shock/boundary layer interaction,” In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, p.4020.
2013, Titchener, N. and Babinsky, H., “Shock wave/boundary-layer interaction control using a combination of vortex generators and bleed,” AIAA J., Vol.51, No.5, pp.1221-1233.
2014, Valdivia, A., Yuceil, K.B., Wagner, J.L., Clemens, N.T. and Dolling, D.S., “Control of supersonic inlet-isolator unstart using active and passive vortex generators,” AIAA J., Vol.52, No.6, pp.1207-1218.
10.2514/1.J0522142024, da Silva Tuan, A.F., Malatesta, V., Silva, A.F.D.C.D. and Jamme, S., “Evaluation of passive control systems for shock wave boundary layer interaction within a supersonic air inlet,” J. Braz. Soc. Mech. Sci. Eng., Vol.46, No.12, p.693.
10.1007/s40430-024-05272-42017, Javed, A. and Chakraborty, D., “Evaluation of side spillage for a hypersonic air intake using computational fluid dynamic techniques,” Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng., Vol.231, No.11, pp.2111-2119.
10.1177/09544100166608732007, Krause, M. and Ballmann, J., “Numerical simulations and design of a scramjet intake using two different RANS solvers,” 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA Paper 2007-5423.
2024, Han, S., Park, Y., Park, J., Nam, J., Lee, B.J. and Lee, H.J., “Numerical investigation of scramjet inlet models for side spillage reduction,” Aerosp. Sci. Technol., Vol.153, p.109423.
10.1016/j.ast.2024.1094232006, Smart, M.K., Hass, N.E. and Paull, A., “Flight data analysis of the HyShot 2 scramjet flight experiment,” AIAA J., Vol.44, No.10, pp.2366-2375.
10.2514/1.206612022, de Siqueira, J.V., Rosa, M.A. and Ribeiro, G.B., “Three-dimensional CFD investigation of a scramjet inlet under different freestream conditions,” Therm. Sci. Eng. Prog., Vol.27, p.101051.
10.1016/j.tsep.2021.1010512016, Arora, N., Ali, M.Y. and Alvi, F.S., “Flowfield of a 3-D swept shock boundary layer interaction in a Mach 2 flow,” 46th AIAA Fluid Dynamics Conference, AIAA Paper 2016-3649.
10.2514/6.2016-36492017, Fang, J., Yao, Y., Zheltovodov, A.A. and Lu, L., “Investigation of three-dimensional shock wave/turbulent-boundary-layer interaction initiated by a single fin,” AIAA J., Vol.55, No.2, pp.509-523.
10.2514/1.J0552831992, Alvi, F.S. and Settles, G.S., “Physical model of the swept shock wave/boundary-layer interaction flowfield,” AIAA J., Vol.30, No.9, pp.2252-2258.
10.2514/3.112121996, Van Oudheusden, B.W., Nebbeling, C. and Bannink, W.J., “Topological interpretation of the surface flow visualization of conical viscous/inviscid interactions,” J. Fluid Mech., Vol.316, pp.115-137.
10.1017/S00221120960004682023, Sabnis, K. and Babinsky, H., “A review of three-dimensional shock wave–boundary-layer interactions,” Prog. Aerosp. Sci., Vol.143, 100953.
10.1016/j.paerosci.2023.1009532023, Khan, A., Chidambaranathan, M., Verma, S.B. and Kumar, R., “Swept shock/boundary-layer interaction control using micro-vortex generators,” Shock Waves, Vol.33, No.7, pp.553-567.
2022, Yang, H., Zong, H., Liang, H., Wu, Y., Zhang, C., Kong, Y. and Li, Y., “Swept shock wave/boundary layer interaction control based on surface arc plasma,” Phys. Fluids, Vol.34, No.8, p.087119.
2013, Liou, M.F. and Lee, B.J., “Mitigation of adverse effects caused by shock wave boundary layer interactions through optimal wall shaping,” 31st AIAA Applied Aerodynamics Conference, AIAA Paper 2013-2653.
10.2514/6.2013-26532004, Park, S.H. and Kwon, J.H., “Implementation of k-ω turbulence models in an implicit multigrid method,” AIAA J., Vol.42, No.7, pp.1348-1357.
10.2514/1.24611981, Roe, P.L., “Approximate Riemann solvers, parameter vectors, and difference schemes,” J. Comput. Phys., Vol.43, No.2, pp.357-372.
10.1016/0021-9991(81)90128-51979, Van Leer, B., “Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method,” J. Comput. Phys., Vol.32, No.1, pp.101-136.
2001, Sung, C.H., Park, S.H. and Kwon, J., “Multigrid diagonalized-ADI method for compressible flows,” 15th AIAA Computational Fluid Dynamics Conference, AIAA Paper 2001-2556.
1994, Menter, F.R., “Two-equation eddy-viscosity turbulence models for engineering applications,” AIAA J., Vol.32, No.8, pp.1598-1605.
10.2514/3.121492021, Young, Y., Han, S. and Park, S., “A study on the internal flowpath separation and bleed rate of the turbine based combined cycle considering back pressure,” J. Comput. Fluids Eng., Vol.26, No.3, pp.34-42.
10.6112/kscfe.2021.26.3.0342023, Ko, B. and Park, S., “Performance analysis of a 3-dimensional dual-path TBCC scramjet intake with bleed control at various flight conditions,” J. Comput. Fluids Eng., Vol.28, No.4, pp.7-15.
10.6112/kscfe.2023.28.4.0072012, Slater, J. W., “Improvements in modeling 90-degree bleed holes for supersonic inlets,” J. Propuls. Power, Vol.28, No.4, pp.773-781.
10.2514/1.591222020, Choe, Y., Kim, C. and Kim, K., “Effects of optimized bleed system on supersonic inlet performance and buzz,” J. Propuls. Power, Vol.36, No.2, pp.211-222.
10.2514/1.B374741995, Willis, B., Davis, D. and Hingst, W., “Flowfield measurements in a normal-hole-bled oblique shock-wave and turbulent boundary-layer interaction,” 31st Joint Propulsion Conference and Exhibit, AIAA Paper 1995-2885.
10.2514/6.1995-2885- Publisher :Korean Society for Computational Fluids Engineering
- Publisher(Ko) :한국전산유체공학회
- Journal Title :Journal of Computational Fluids Engineering
- Journal Title(Ko) :한국전산유체공학회지
- Volume : 31
- No :2
- Pages :84-103
- Received Date : 2026-04-07
- Revised Date : 2026-06-19
- Accepted Date : 2026-06-23
- DOI :https://doi.org/10.6112/kscfe.2026.31.2.084


Journal of Computational Fluids Engineering








