[1] 彭志琦, 张均锋, 牛斌. 曲率半径对前缘气动热与结构响应的影响. 力学与实践2011, 33(2): 18-23 Peng Zhiqi, Zhang Junfeng, Niu Bin. Influences of curvature radius of leading edge on aerodynamic heating and structural response.Mechanics in Engineering, 2011, 33(2): 18-23 (in Chinese) [2] Boman B, Elias T. Tests on a sodium/Hastelloy X wing leading edge heat pipe for hypersonic vehicles. 5th Joint Thermophysics and Heat Transfer Conference, Seattle, WA, 2013 [3] 张志成. 高超声速气动热和热防护. 北京: 国防工业出版社, 2003 Zhang Zhicheng. Hypersonic Aerodynamic Heating and Thermal Protection. Beijing: National Defense Industry Press, 2003 (in Chinese) [4] Van Driest ER. The problem of aerodynamic heating.Aeronautical Engineering Review, 1956, 15(10): 26-41 [5] 殷金其. 航天热防护材料的烧蚀特性研究. 固体火箭技术, 1993(4): 84-91 Yin Jinqi. Study of ablative characteristics of materials used for space thermal protection system.Journal of Solid Rocket Technology, 1993(4): 84-91 (in Chinese)[6] Wen G, Sui SH, Song L, et al. Formation of ZrC ablation protective coatings on carbon material by tungsten inert gas cladding technique. Corrosion Science, 2010, 52(9): 3018-3022 [7] Zhu K, Li Y, Lu P. Experimental investigation on heat transfer characteristics of a novel heat pipe radiator used to cool high heat flux device.Cryogenics & Superconductivity, 2011, 39(1): 42-46 [8] Li QH, Zhao XB, Huang H, et al. A multistage cool storage system of natural coldness resource based on heat pipe.Advanced Materials Research, 2012, 512-515: 1097-1101 [9] Gwon HS, Kim SH, Kasada R, et al. Anisotropic heat transfer characteristics of composite material enhanced with high thermal conductivity fiber. 25th Symposium on Fusion Engineering, San Francisco, CA, 2013 [10] Silverstein CC. A feasibility study of dredged leading edges for hypersonic cruise aircraft. NASA CR 1857, 1971 [11] Niblock GA, Reeder JC, Huneidi F. Four space shuttle wing leading edge concepts.Journal of Spacecraft and Rockets, 1974, 11(5): 314-320 [12] Xie G, Ji T, Sunden B, et al. Investigation on thermal performance of a high-temperature heat-pipe thermal protection structure.Journal of Engineering Thermophysics, 2016, 25(3): 359-376 [13] 赵蔚琳, 刘宗明, 李树人. 高温热管的研究与发展. 石油化工设备, 200534(4): 40-44 Zhao Weilin, Liu Zongming, Li Shuren. Research and development of high temperature heat pipes.Petro-chemical Equipment, 2005, 34(4): 40-44 (in Chinese) [14] 刘洪鹏, 刘伟强. 飞行器层板式前缘热管防热结构等效热分析. 国防科技大学学报, 2016, 38(2): 19-24 Liu Hongpeng, Liu Weiqiang. Effective thermal analysis of platelet heat-pipe-cooled leading edge of vehicle.Journal of National University of Defense Technology, 2016, 38(2): 19-24 (in Chinese) [15] 陈连忠, 欧东斌. 高温热管在热防护中应用初探. 实验流体力学, 20103(2): 51-54 Chen Lianzhong, Ou Dongbin. Elementary research on the application of high temperature heat-pipe to the thermal protection.Journal of Experiments in Fluid Mechanics, 2010, 3(2): 51-54 (in Chinese) |