| Citation: | JIANG Peixue, ZHANG Fuzhen, XU Ruina, ZHU Yinhai. Integrated thermal protection and power generation system of hypersonic vehicle engine[J]. Journal of Aerospace Power, 2021, 36(1): 1-7. doi: 10.13224/j.cnki.jasp.2021.01.001
|
| [1] |
SUTTON G P,BIBLARZ O.Rocket propulsion elements［M］.Hoboken,New Jersey:John Wiley and Sons,2016.
|
| [2] |
牛文敬,连文磊,林灵矫.基于热管技术的飞机电作动机构散热特性［J］.航空动力学报,2020,35(4):711-721. NIU Wenjing,LIAN Wenlei,LIN Lingjiao,et al.Cooling performance of electric actuating mechanism on,aircrafts based on heat pipes［J］.Journal of Aerospace Power,2020,35(4):711-721.(in Chinese)
|
| [3] |
韩海涛,陈智,胡龙飞,等.基于高温热管的超燃燃烧室热防护结构［J］.航空动力学报,2017,32(5):1043-1050. HAN Haitao,CHEN Zhi,HU Longfei,et al.High temperature heat pipe enhanced thermal protection structure for scramjet combustion chamber［J］.Journal of Aerospace Power,2017,32(5):1043-1050.(in Chinese)
|
| [4] |
马坤,朱亮,陈雄.高超声速流场支杆射流减阻降热的流热耦合［J］.航空动力学报,2020,35(4):793-804. MA Kun,ZHU Liang,CHEN Xiong.Fluid-thermal coupling on drag and heat reduction induced by spike and jet in hypersonic flow field［J］.Journal of Aerospace Power,2020,35(4):793-804.(in Chinese)
|
| [5] |
闫帅,祝银海,姜培学,等.超临界压力下正癸烷在多孔介质中结焦实验研究［J］.推进技术,2018,39(4):935-941. YAN Shuai,ZHU Yinhai,JIANG Peixue,et al.Experiment on coke deposition of supercritical n-decane in porous media［J］.Journal of Propulsion Technology,2018,39(4):935-941.(in Chinese)
|
| [6] |
熊宴斌,祝银海,姜培学,等.单相液体发汗冷却规律实验［J］.航空动力学报,2013,28(9):1956-1961. XIONG Yanbin,ZHU Yinhai,JIANG Peixue et al.Experiment of transpiration cooling rules of single phase liquid［J］.Journal of Aerospace Power,2013,28(9):1956-1961.(in Chinese)
|
| [7] |
SEGAL C.The scramjet engine:processes and characteristics［M］.Cambridge,UK:Cambridge University Press,2009.
|
| [8] |
鲍文,秦江,于达仁,等.回热式闭式布莱顿超燃冲压发动机冷却循环系统:CN 101576024A［P］.2009-11-11.
|
| [9] |
QIN J,ZHOU W X,BAO W,et al.Thermodynamic analysis and parametric study of a closed Brayton cycle thermal management system for scramjet［J］.International Journal of Hydrogen Energy,2010,35(1):356-364.
|
| [10] |
李新春,王中伟.高超声速飞行器的热电技术热管理系统参数［J］.国防科技大学学报,2016,38(2):43-47,86. LI Xinchun,WANG Zhongwei.Parametric of an integrated thermoelectric generation thermal management system for hypersonic vehicle［J］.Journal of National University of Defense Technology,2016,38(2):43-47,86.(in Chinese)
|
| [11] |
李新春,王中伟.超燃冲压发动机壁面热量的利用潜力分析［J］.推进技术,2017,38(2):275-280. LI Xinchun,WANG Zhongwei.Analysis of potential usage for heat of scramjet wall［J］.Journal of Propulsion Technology,2017,38(2):275-280.(in Chinese)
|
| [12] |
张富珍,姜培学,胥蕊娜,等.基于回热器温度滑移匹配的以CO2为工质的布雷顿循环优化分析［J］.热能动力工程,2017,32(8):11-16. ZHANG Fuzhen,JIANG Peixue,XU Ruina,et al.Optimization analysis of a Brayton cycle using CO2 as working substance based on temperature glide matching in heat exchanger［J］.Journal of Engineering for Thermal Energy and Power,2017,32(8):11-16.(in Chinese)
|
| [13] |
ZHANG F Z,ZHU Y H,LI C H,et al.Thermodynamic optimization of heat transfer process in thermal systems using CO2 as the working fluid based on temperature glide matching［J］.Energy,2018,151:376-386.
|
| [14] |
FEHER E G.The supercritical thermodynamic power cycle［J］.Energy Conversion,1968,8(2):85-90.
|
| [15] |
AHN Y,LEE J,KUM S G,et al.Design consideration of supercritical CO2 power cycle integral experiment loop［J］.Energy,2015,86:115-127.
|
| [16] |
AHN Y,BAE S J,KIM M,et al.Review of supercritical CO2 power cycle technology and current status of research and development［J］.Nuclear Engineering and Technology,2015,47(6):647-661.
|
| [17] |
PASCH J,CONBOY T,FLEMING D,et al.Supercritical CO2 recompression Brayton cycle:complete assembly description［R］.Sandia Report,SAND2012-9546,2012.
|
| [18] |
UTAMURA M,HASUIKE H,OGAWA K,et al.Demonstration of supercritical CO2 closed regenerative Brayton cycle in a bench scale experiment［R］.ASME Paper GT2012-68697,2012.
|
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