| [1] 蒋友娣, 董葳, 陈勇. 高超声速钝头体变熵流表面热流计算[J]. 航空动力学报, 2008, 23(9):1396-1398. JIANG Y D, DONG W, CHEN Y. Surface heat flux calculation of variable entropy flow for hypersonic blunt bodies[J]. Journal of Aerospace Power, 2008, 23(9):1396-1398(in Chinese).
[2] 蒋友娣, 董葳, 陈勇. 高超声速飞行器瞬态表面热流和温度的工程计算[J]. 能源技术, 2007, 28(6):316-318. JIANG Y D, DONG W, CHEN Y. Transient surface heat flux and surface temperature engineering prediction of hypersonic vehicle[J]. Energy Technology, 2007, 28(6):316-318(in Chinese).
[3] CAYZAC R, GRIGNON C, CARETTE E.Navier-Stokes computation of heat transfer and aero-heating modeling for supersonic projectiles[J].Aerospace Science and Technology, 2006, 10(5):374-384.
[4] 孙兆虎. 高超声速飞行器结构热问题讨论[J]. 航空科学技术, 2008, 3(2):13-16. SUN Z H. The issues of the aerodynamic heating and thermal protection of hypersonic flight vehicle[J]. Aeronautical Science and Technology, 2008, 3(2):13-16(in Chinese).
[5] 张伟, 张正平, 李海波, 等. 高超声速飞行器结构热试验技术进展[J]. 强度与环境, 2011, 38(1):1-7. ZHANG W, ZHANG Z P, LI H B, et al. Progress on thermal test technique of hypersonic vehicle structures[J]. Structure & Environment Engineering, 2011, 38(1):1-7(in Chinese).
[6] 吴大方, 潘兵, 高镇同, 等. 超高温、大热流、非线性气动热环境试验模拟及测试技术研究[J]. 实验力学, 2012, 27(3):256-269. WU D F, PAN B, GAO Z T, et al. On the experimental simulation of ultra-high temperature, high heat flux and nonlinear aerodynamic heating environment and thermo-machanical testing technique[J]. Journal of Experimental Mechanics, 2012, 27(3):256-269(in Chinese).
[7] GAS F, JOHN W, CHARLES B.Thin film heat flux sensor of improved design:NASA/TM-2002-211566[R].Washington. D. C:NASA, 2002.
[8] LARRY H, CRAIG S. X-37 C/SiC ruddervator subcomponent test program[C]//Annual Meeting, Washington. D. C:NASA, 2009:12-13.
[9] FERDINAND W G, STEPHEN A R, Chad E R. Dynamic response of X-37 hot structure control surfaces exposed to controlled reverberant acoustic excitation:NASA/TM-2005-2010[R].Washington. D. C:NASA. 2005.
[10] ANTHONY P, LANCE W R, HUDSON L D.High-temperature strain sensing temperature strain sensing for aerospace applications[C].//Summer WRSGC, Washington. D. C:NASA. 2008:22-25.
[11] 王安龄, 桂业伟, 贺立新, 等. 采用非均匀防热材料进行高速飞行器防热设计的防热效果研究[J]. 工程热物理学报, 2007, 28(4):655-657. WANG A L, GUI Y W, HE L X, et al. Study on heat prevention effects of the heterogeneous material for hypersonic vehicle[J]. Journal of Engineering Thermophysics, 2007, 28(4):655-657(in Chinese).
[12] 曹志松, 刘绍然, 裴一飞. 卫星虚拟热试验平台建模工具模块研究[J]. 航天器环境工程, 2012, 29(1):42-45. CAO Z S, LIU S R, PEI Y F. Tool module for modeling satellite virtual thermal test platform[J]. Spacecraft Environment Engineering, 2012, 29(1):42-45(in Chinese).
[13] 康宏琳, 阎超, 李亭鹤, 等. 高超声速再入钝头体表面热流计算[J]. 北京航空航天大学学报, 2006, 32(12):1395-1398. KANG H L, YAN C, LI T H, et al. Numerical study of aero heating predictions for hypersonic reentry bodies[J]. Journal of Beijing University of Aeronautics and Astronautics, 2006, 32(12):1395-1398(in Chinese).
[14] 何西波, 崔占中, 王智勇. 热试验中的混合温度控制法研究[J]. 强度与环境, 2009, 36(5):43-46 HE X B, CUI Z Z, WANG Z Y. Research of compound temperature control in thermal test[J]. Structure & Environment Engineering, 2009, 36(5):43-46(in Chinese).
[15] 帅永, 齐宏, 谈和平. 热辐射测量技术[M]. 哈尔滨:哈尔滨工业大学出版社. 2009:34-39. SHUAI Y, QI H, TAN H P. Measurement technique on thermal radiation[M]. Harbin:Harbin Institute of Technology Press, 2009:34-39(in Chinese). |
CJA
