LI S X. Complicated flow governed by shock and boundary layer[M]. Beijing:Science Press, 2007. (in Chinese)

BABINSKY H, HARVEY J K. Shock wave-boundary-layer interactions[M]. Cambridge University Press, 2011.

ZHANG Z C. Hypersonic aerothermodynamic and thermal protection[M]. Beijing:National Defence Industry Press, 2003. (in Chinese)

BERTIN J J, CUMMINGS R M. Critical hypersonic aerothermodynamic phenomena[J]. Annual Review of Fluid Mechanics, 2006, 38(1):129-157.

LI J W, WANG Q, ZHAO W. Investigation on aerodynamic heating characteristics of hypersonic flat pate/cylinder juncture flow[J]. Journal of North University of China, 2017, 38(5):609-613. (in Chinese)

JIA W L, LUO J L, KANG H L. Aerodynamic heating of the gap between aircraft wing and rudder[C]//The 18th National Conference on Shock Wave and Shock Tube, 2018. (in Chinese)

CHEN J Y, YAN C. Numerical simulation of flow in rudder gap[C]//Proceeding of 15th Computational Fluid Dynamics Symposium. Beijing: Chinese Society of Theoretical and Applied Mechanics, 2012: 777-781. (in Chinese)

SI Y. Thermal environment and thermal protection research of local area between control-flap and maneuver vehicle[M]. Beijing: Beijing University of Aeronautics and Astronautics, 2013. (in Chinese)

ZHOU J. Study of aerodynamic heating environment on blunt-fin gap of hypersonic vehicle[M]. Mianyang: Southwest University, 2014. (in Chinese)

BUR R, CHANETZ B. Experimental study on the PRE-X vehicle focusing on the transitional shock-wave/boundary-layer interactions[J]. Aerospace Science and Technology, 2009, 13(7):393-401.

TAN J, TU J Q, SUN X F, et al. Numerical study of hypersonic shock-wave/laminar boundary-layer interactions of a typical lifting vehicle[R]. AIAA 2017-3288.

KNIGHT D, MORTAZAVI M. Hypersonic shock wave transitional boundary layer interactions-A review[R]. AIAA 2017-312.