| Citation: | ZHANG Jun-feng, MU Dan, BIAN Xiang-de. Design analysis of active cooling composite combustion chamber with thin wall[J]. Journal of Aerospace Power, 2013, 28(11): 2401-2407.
|
| [1] |
Clément B,Roger F,Agnès L,et al.Fully ceramic composite heat exchanger qualification for advanced combustion chambers.AIAA-2005-3433,2005.
|
| [2] |
Clément B,Alain L.Ceramic matrix composites cooled panel development for advanced propulsion systems// 45th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference.Palm Springs,US:AIAA,2004:19-22.
|
| [3] |
Marc B,Steffen B.PTAH-SOCAR fuel-cooled composite materials structure for dual-mode ramjet and liquid rocket engines:2005 status//AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies.Capua,Italy:AIAA,2005:1-11.
|
| [4] |
Marc B,Steffen B.PTAH-SOCAR fuel cooled composite materials structure for dual-mode ramjet and liquid rocket engines//40th AIAA/ASME/ASAE/ASEE Joint Propulsion Conference and Exhibit.Fort Lauderdale,US:AIAA,2004:11-14.
|
| [5] |
Alber H B.Hypersonic air-breathing propulsion efforts in the air force research laboratory.AIAA-2005-3255,2005.
|
| [6] |
Joseph M H,James S M,Richard C M.The X-51A scramjet engine flight demonstration program.AIAA-2008-2540,2008.
|
| [7] |
Lorenzo V,Natasha V,Kathryn H,et al.Design of actively cooled panels for scramjets.AIAA-2006-8069,2006.
|
| [8] |
Dennis H P,Stuart C J,William M D.Integrated numerical methods for hypersonic aircraft cooling systems analysis.AIAA 92-0254,1992.
|
| [9] |
吴峰,王秋旺,罗来勤,等.液体推进剂火箭发动机推力室再生冷却通道三维流动与传热数值计算[J].航空动力学报,2005,20(4):707-712. WU Feng,WANG Qiuwang,LUO Laiqin,et al.Numerical simulation of heat transfer and fluid flow in cooling channel of the liquid rocket engine thrust chamber[J].Journal of Aerospace Power,2005,20(4):707-712.(in Chinese)
|
| [10] |
吴峰,王秋旺,罗来勤,等.液体火箭发动机推力室冷却通道传热优化计算[J].推进技术,2006,27(3):197-200. WU Feng,WANG Qiuwang,LUO Laiqin,et al.Numerical optimization simulation on heat transfer in cooling channel of H2/O2 liquid rocket engine thrust chamber[J].Journal of Propulsion Technology,2006,27(3):197-200.(in Chinese)
|
| [11] |
吴峰,曾敏,王秋旺,等.通道深宽比对液体火箭发动机推力室再生冷却的影响[J].航空动力学报,2007,22(1):114-118. WU Feng,ZENG Min,WANG Qiuwang,et al.Effect of aspect ratio on heat transfer and fluid flow in regenerative cooling channel of liquid rocket engine thrust chamber[J].Journal of Aerospace Power,2007,22(1):114-118.(in Chinese)
|
| [12] |
彭丽娜,何国强,刘佩进,等.耐高温复合材料的主动冷却实验和数值计算研究[J].宇航学报,2008,29(5):1668-1672. PENG Lina,HE Guoqiang,LIU Peijin,et al.Experiments and numerical nimulation of active cooling ceramic matrix composite[J].Journal of Astronautics,2008,29(5):1668-1672.(in Chinese)
|
| [13] |
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,2009,30(5):513-517. ZHONG Fengquan,FAN Xuejun,YU Gang.Heat transfer analysis for actively cooled supersonic combustor[J].Journal of Propulsion Technology,2009,30(5):513-517.(in Chinese)
|
| [14] |
郭运强.某型发动机火箭筒非均匀温度场下热应力分析.西安:西北工业大学,2004. GUO Yunqiang.Thermal stress analysis of a combustor of gas turbine engine under inhomogeneous high temperature.Xi'an:Northwestern Polytechnical University,2004.(in Chinese)
|
| [15] |
彭志琦,张均锋,牛斌,等.曲率半径对前缘气动热与结构响应的影响[J].力学与实践,2011,33(2):18-23. PENG Zhiqi,ZHANG Junfeng,NIU Bin,et al.Influences of curvature radius of leading edge on aerodynamic heating and structural response[J].Mechanics in Engineering,2011,33(2):18-23.(in Chinese)
|
| [16] |
彭志琦.前缘类构件的热结构分析及参数影响规律研究.北京:中国科学院,2011. PENG Zhiqi.Thermal structure analysis of leading edge and influences of parameters.Beijing:Chinese Academy of Sciences,2011.(in Chinese)
|
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