Calculation of thermal load and impact factor analysis for hypersonic vehicle

[1] 范绪箕.气动加热与热防护系统[M].北京:科学出版社,2004: 75-129 Fan Xuji. Aeroheating and thermal protection system[M]. Beijing: Science Press, 2004: 75-129(in Chinese) [2] 王浚,王佩广. 高超声速飞行器一体化防热与热控设计方法[J]. 北京航空航天大学学报, 2006, 32(10):1129-1134 Wang Jun, Wang Peiguang. Integrated thermal protection and control design methodology for hypersonic vehicles[J].Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(10):1129-1134(in Chinese) [3] 杨世铭,陶文铨.传热学[M].北京:高等教育出版社,1998:71-80 Yang Shiming, Tao Wenquan. Heat transfer[M]. Beijing: China Higher Education Press, 1998:71-80(in Chinese) [4] 李运泽,魏传锋,袁领双,等. 卫星热控系统的动态特性建模与仿真[J]. 北京航空航天大学学报, 2005, 31(3):372-374 Li Yunze, Wei Chuanfeng, Yuan Lingshuang, et al. Dynamical modeling and simulation of satellite thermal control system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(3): 372-374(in Chinese) [5] Kleb W L, Wood W A, Gnoffo P A. Computational aeroheating predictions for X-34 . AIAA-98-0879, 1998 [6] Wurster K E, Riley C J, Zoby E V. Engineering aerothermal analysis for X-34 thermal protection design . AIAA-98-16690, 1998 [7] Brauckmann G J. X-34 vehicle aerodynamic characteristics . AIAA-98-32431, 1998 [8] Tang Lei, Wei Shyy, Utturkar Y, et al. Proper orthogonal decomposition and response surface method for TPS/RLV structural design and optimization: X-34 case study . AIAA-2005-839, 2005 [9] Riley C J, Kleb W L. Aeroheating predictions for X-34 using an inviscid-boundary layer method . AIAA-98-0880, 1998