Bertin JJ,Cummings RM.Critical hypersonic aerothermodynamic phenomena.Annual Review of Fluid Mechanics,2006,38:129-157
|
Holden MS.Design,development and calibration of the LENS facility.AFOSR-TR.1994,940161
|
Dunn MG,Moller JC,Steele RC.Development of a new high-enthalpy shock tunnel.AIAA-88-2782,1988
|
钱学森.我对今日力学的认识.力学与实践,1995,17(4):1 (Tsien Hsue-shen.My cognition on today's mechanics. Mechanics and Practice,1995,17(4):1 (in Chinese))
|
Holden MS,Parker R.LENS hypervelocity tunnels and application to vehicle testing at duplicated conditions.In:Advanced Hypersonic Test Facilities.Lu F,Marren D,eds.Progress in Astronautics and Aeronautics,Volume 198.AIAA,2002
|
Fickett W,Davis WC.Detonation Theory and Experiment.Mineola.New York:Dover Publications,INC.1979
|
Yu HR,Esser B,Lenartz M,et al.Gaseous detonation driver for a shock tunnel.Shock Waves,1992,2 (4):245-254
|
张欣玉,俞鸿儒,赵伟等.氢氧爆轰直接起始实验研究.流体力学测量与控制,1996,10(3):63-68 (Zhang Xinyu,Yu Hongru,Zhao Wei,et al.Turbulent jet initiation of oxy-hydrogen direct detonation.Aerodynamic Experiment and Measurement and Control,1996,10(2):63-68 (in Chinese))
|
赵伟,俞鸿儒.过临界喷管充气混合装置.空气动力学学报,1999,17(3):279-284 (Zhao Wei,Yu Hongru.The double over-critical nozzles device for filling and mixing mixture gases.Acta Aerodynamica Sinica,1999,17(3):279-284 (in Chinese))
|
Lu FK,Wilson DR,Bakos RJ,et al.Recent advances in detonation techniques for high-enthalpy facilities.AIAA Journal,2000,38 (9):1676-1684
|
Jiang ZL,Zhao W,Wang C,et al.Study on forward detonation driver for high enthalpy shock tunnels.AIAA Journal,2002,40(10):2009-2016
|
Flagg RF.Detailed analysis of shock tube tailored conditions.RAD-TM-63-64,1963
|
李进平,冯珩,姜宗林等.爆轰驱动激波管缝合激波马赫数计算.空气动力学学报,2008,26 (3):291-296 (Li Jinping,Feng Heng,Jiang Zonglin,et al.Numerical computation on the tailored shock mach numbers for a hydrogen-oxygen detonation shock tube.Acta Aerodynamica Sinica,2008,26 (3):291-296 (in Chinese))
|
俞鸿儒,林建民,李仲发等.扩张激波管流动波图观察.空气动力学学报,1984,3:88-91 (Yu Hongru,Lin Jianmin,Li Zhongfa,et al.Observation of wave diagrams for shock tube with the divergent nozzle at diaphragm section.Acta Aerodynamica Sinica,1984,3:88-91 (in Chinese))
|
Laderman AL.Shock-tube performance with area divergence at the diaphragm section.AIAA Journal,1967,10:1904-1906
|
赵伟,姜宗林,俞鸿儒.高焓激波风洞爆轰驱动技术研究.空气动力学学报,2009,27:63-68 (Zhao Wei,Jiang Zonglin,Yu Hongru.Study on detonation drivers for high-enthalpy shock tunnels.Acta Aerodynamica Sinica,2009,27:63-68 (in Chinese))
|
李进平,冯珩,姜宗林.激波/边界层相互作用诱导的激波风洞气体污染问题.力学学报,2008,40(3):289-296 (Li Jinping,Feng Heng,Jiang Zonglin.Gas contamination induced by the interaction of shock/boundary layer in shock tunnel.Chinese Journal of Theoretical and Applied Mechanics,2008,40(3):289-296 (in Chinese))
|
Burtschell Y,Cardoso M.Numerical analysis of reducing driver gas contamination in impulse shock tunnels.AIAA Journal,2001,39:2357-2365
|