| Citation: | HUANG Xi-qiao, CHEN Le, YAN Chuan-jun, ZHENG Long-xi, WANG Zhi-wu, QIU Hua. Experiment on heating kerosene with useless heat on the wall of pulse detonation engine[J]. Journal of Aerospace Power, 2011, 26(8): 1702-1707.
|
| [1] |
严传俊,范玮,黄希桥,等.脉冲爆震发动机原理及关键技术[M].西安:西北工业大学出版社,2005:277-280.
|
| [2] |
严传俊,范玮,黄希桥,等.现概念脉冲爆震发动机的探索性研究[J].自然科学进展,2002,12(10):1021-1025. YAN Chuanjun,FAN Wei,HUANG Xiqiao,et al.New concept of pulse detonation engine exploratory study[J].Progress in Natural Science,2002,12(10):1021-1025.(in Chinese)
|
| [3] |
郑龙席,严传俊,范玮,等.脉冲爆震发动机模型机爆震室壁温分布实验研究[J].燃料科学与技术,2003,9(4):344-347. ZHENG Longxi,YAN Chuanjun,FAN Wei,et al.Experimental investigation on outer wall temperature distribution of a pulse detonation engine model[J].Journal of Combustion Science and Technology,2003,9(4):344-347.(in Chinese)
|
| [4] |
Miser C L,King P I.PDE flash vaporization system for hydrocarbon fuel using thrust tube waste heat.AIAA Paper 2005-3511,2005.
|
| [5] |
Tucker K C,King P I.The use of a flash vaporization system with liquid hydrocarbon fuels in pulse detonation engine.AIAA Paper 2004-868,2004.
|
| [6] |
Helfrich T M,King P I.Effect of supercritical fuel injection on cycle performance of pulsed detonation engine[J].Journal of Propulsion and Power,2007,23(4):748-755.
|
| [7] |
Stevens C A,King P I.Fuel composition and coking analysis of endothermically heated hydrocarbon fuels for use in a pulsed detonation engine.AIAA Paper 2009-501,2009.
|
| [8] |
Ghosn L J,Zhu D.Thermal barrier and protective coating to improve the durability of a combustor under apulse detonation engine environment.AIAA Paper 2007-2070,2007.
|
| [9] |
Ajmani K,Breisacher K J.Qualitative study of cooling methods for a pulse detonation engine.Lake Buena Vista,Florida:51st JANNAF Propulsion Meeting,2002.
|
| [10] |
Ajmani K,Breisacher K J.Multi-cycle analysis of an ejector-cooled pulse detonation device.AIAA Paper 2004-3915,2004.
|
| [11] |
Ajmani K,Breisacher K J.Numerical an experimental studies of a film cooled pulsed detonation tube.AIAA Paper 2005-3509.2005.
|
| [12] |
涂洪妍,范玮.基于主动冷却的脉冲爆震火箭发动机试验研究.西安:西北工业大学,2010. TU Hongyan,FAN Wei.Experiment of pulse detonation rocket engines based on active cooling.Xi'an:Northwestern Polytechnical University,2010.(in Chinese)
|
| [13] |
宫继双,范育新,王家骅,等.爆震管壁面热负荷实验[J].航空动力学报,2009,24(9):1952-1958. GONG Jishuang,FAN Yuxin,WANG Jiahua,et al.Experimental study on heat load of detonation tube[J].Journal of Aerospace Power,2009,24(9):1952-1958.(in Chinese)
|
| [14] |
陈乐,黄希桥,严传俊,等.燃油温度对PDE性能的影响实验[J].西北工业大学学报,2010,28(5):649-654. CHEN Le,HUANG Xiqiao,YAN Chuanjun,et al.Exploring Experimentally effect of kerosene temperature on performance of pulse detonation engine (PDE)[J].Journal of Northwestern Polytechnical University,2010,28(5):649-654.(in Chinese)
|
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