[1] Lander H,Nixon A C.Endothermic Fuels for Hypersonic Vehicles[J].Journal of Aircraft, 1971,8(4):200-207.
[2] Yang V.Modeling of Supercritical Vaporization, Mixing and Combustion Processes in Liquid-Fueled Propulsion System[J].Proceeding of the Combustion Institute, 2000,8:925-942.
[3] Linne D L,Meyer M L, Edwards T, et al.Evaluation of Heat Transfer and Thermal Stability of Supercritical JP-7Fuel [R].AIAA 97-3041.
[4] Hitch B, Karpuk M.Experimental Investigation of Heat Transfer and Flow Instability in Supercritical Fuels [R].AIAA 97-3043.
[5] Edwards T, Maurice L Q.Surrogate Mixtures to Represent Complex Aviation and Rocket Fuels[J].Journal of Propulsion and Power, 2001,7:461-466.
[6] Edwards T,Anderson S.Results of High Temperature JP-7Cracking Assessment[R].AIAA 93-0806.
[7] 胡志宏, 陈听宽, 罗毓珊, 等.高热流条件下超临界压力煤油流过小直径管的传热特性[J].化工学报, 2002,3(2).
[8] 罗毓珊, 陈听宽, 胡志安, 等.高参数小管径内煤油的传热特性研究[J].工程热物理学报, 2005,6(4).
[9] Zhong F, Fan X, Yu G, et al.Heat Transfer of Aviation Kerosene at Supercritical Conditions[R].AIAA 2008-4615.
[10] 范学军, 俞刚.大庆RP-3航空煤油热物性分析[J].推进技术, 2006,7(2).(FAN Xue-jun, YU Gang.Analysis of Thermophysical Properties of Daqing RP-3Aviation Kerosene[J].Journal of Propulsion Technology, 2006,7(2).)
[11] 仲峰泉, 范学军, 俞刚.带主动冷却的超声速燃烧室传热分析[J].推进技术, 2009,0(5).(ZHONG Feng-quan, FAN Xue-jun, Yu Gang.Heat Transfer Analysis for Actively Cooled Supersonic Combustor[J].Journal of Propulsion Technology, 2009,0(5).)
[12] Li X F, Zhong F Q, Fan X J, et al.Study of Turbulent Heat Transfer of Aviation Kerosene Flows in a Curved pipe at Supercritical Pressure[J].Applied Thermal Engineering, 2010,0:1845-1851.
[13] Haijun Wang, Yushan Luo, Hongfang Gu,et al.Experimental Investigation on Heat Transfer and Pressure Drop of Kerosene at Supercritical Pressure in Square and Circular Tube with Artificial Roughness[J].Experimental Thermal and Fluid Science, 2012,2:16-24.
[14] Xunfeng Li, Xiulan Huai, Jun Cai, et al.Convective Heat Transfer Characteristics of China RP-3Aviation Kerosene at Supercritical Pressure[J].Applied Thermal Engineering, 2011,1:2360-2366.
[15] Dang GuoXin, Zhong FengQuan, Chen LiHong,et al.Numerical Investigation on Flow and Convective Heat Transfer of Aviation Kerosene at Supercritical Conditions[J].Science China, 2013,6(2):416-422.
[16] 李勋锋, 仲峰泉, 范学军.超临界压力下航空煤油圆管流动和传热的数值研究[J].推进技术, 2010,1(4).(LI Xun-feng,ZHONG Feng-quan,FAN Xue-jun.Numerical Study of Convective Heat Transfer of Aviation Kerosene Flows in Pipe at Supercritical Pressure[J].Journal of Propulsion Technology, 2010,1(4).)
[17] 李勋锋, 仲峰泉, 范学军.超临界压力下航空煤油水平管内对流换热特性数值研究[J].航空动力学报,2010,5(8).
[18] 王曦, 仲峰泉, 陈立红,等.考虑煤油裂解效应的超声速燃烧室再生冷却过程分析[J].推进技术, 2013,4(1).(WANG Xi, ZHONG Feng-quan, CHEN Li-hong, et al.A Coupled Heat Transfer Analysis with Effects of Catalytic Cracking of Kerosene for Actively Cooled Supersonic Combustor[J].Journal of Propulsion Technology, 2013,4(1).)
[19] 杨世铭, 陶文铨.传热学[M].北京:高等教育出版社,2006.
[20] 华绍曾, 杨学宁.实用流体阻力手册[M].北京:国防工业出版社,1985.
|