Heiser W H, Pratt D T. Hypersonic air breathing propulsion [M]. Washington, D C:American Institute of Aeronautics and Astronautics, 1994: 3―26.
[2]
Taylor H D. The elimination of diffuser separation by vortex generators [R]. United Aircraft Corporation Report No. R-4012-3, June, 1947.
[3]
Bragg M B, Gregorek G M. Experimental study of airfoil performance with vortex generators [J]. Journal of Aircraft, 1987,24(5):305―309.
[4]
Calarese W, Crisler W P, Gustsfson G L. Afterbody drag reduction by vortex generators [R]. Reno, N V:AmericanInstitute of Aeronautics and Astronautics, 1985.
[5]
Rao D M, Kariya T T. Boundary layer submerged vortex generators for separation control an exploratory study [R]. Cincinati, OH, American Institute of Aeronautics and Astronautics, 1988.
[6]
McCormick D C. Shock-boundary layer interaction control with low-profile vortex generators and passive cavity [R]. Reno, N V:AmericanInstitute of Aeronautics and Astronautics, 1992.
[7]
Kim J Q, Ryou H S, Jeong J Y,et al. Numerical simulation of 3-D turbulent flow with imbedded longitudinal vortex [J]. Computational Fluid Dynamics Journal, 1996,4(4):473―488.
[8]
Yang J S, Seo J K, Lee K B. A number analysis on flow field and heat transfer by interaction between a pair of vortices in rectangular channel flow [J]. Current Applied Physics, 2001,1(4/5):393―405.
[9]
Lee S, Loth E, Wang C. LES of supersonic turbulent boundary layers with μVGs [R]. Miami, Florida, American Institute of Aeronautics and Astronautics, 2007.
[10]
Babinsky H, Li Y, C. W. Pitt Ford. Microramp control of supersonic oblique shock-wave/boundary layer interactions [J]. American Institute of Aeronautics and Astronautics Journal, 2009,47(3):668―675.
[11]
Li Qin, Liu Chaoqun. LES for supersonic ramp control flow using MVG at Ma =2. 5 and Reθ, =1440 [R]. Orlando, Florida, American Institute of Aeronautics and Astronautics, 2010.
[12]
Kim J, Kim D, Choi H. An immersed boundary finite volume method for simulations of flow in complex geometries [J]. Journal of Computational Physics, 2001,171:132―150.
[13]
Berger M, Colella P. Local adaptive mesh refinement for shock hydrodynamics[J]. Journal of Computer &Physics, 1988,82:64―84.