Citation: | Yu Nanjia, Cai Guobiao, Zhang Guozhouet al. Gas dynamic resonance performance of coaxial injector[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(1): 82-86. (in Chinese) |
[1] Rocketdyne Engineering.Advanced ignition systems final report .N71-35152,1972 [2] Thompson P A.Jet-driven resonance tube[J].J AIAA,1964,2(7):1230-1233 [3] Przirembel C E G,Fletcher L S.The aerothermodynamics of a simple resonance tube .AIAA75-0687,1975 [4] 张涵信.无波动、无自由参数的耗散差分格式[J].空气动力学学报,1988,6(2):143-164 Zhang Hanxin.Non oscillatory and non free parameter dissipation difference scheme[J].Acta Aerodynamic,1988,6(2): 143-164(in Chinese) [5] 郑敏,张涵信.无波动、无自由参数的耗散差分格式(NND)在喷管计算中的应用[J].空气动力学学报,1989,7(3):273-281 Zheng Min,Zhang Hanxin.Application of non oscillatory and non free parameters dissipative finit difference scheme to the calculation of free jet flows[J].Acta Aerodynamic,1989,7(3):273-281(in Chinese) [6] 俞南嘉,张国舟,宋雅娜.气动谐振加热基础试验 [J].航空动力学报,2005,20(2):323-327 Yu Nanjia,Zhang Guozhou,Song Yana.Experimental investigation of gas-dynamic resonance heating [J].Journal of Aerospace Power,2005,20(2):323-327(in Chinese) [7] 俞南嘉,张国舟,宋雅娜,等.同轴氢氧谐振点火器试验研究 [J].推进技术,2004,25(3):267-270 Yu Nanjia,Zhang Guozhou,Song Yana,et al.Experimental investigation for coaxial hydrogen/oxygen resonance ignitor [J].Journal of Propulsion Technology,2004,25(3):267-270(in Chinese)
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