[1]胡晓磊,李仁凤,谢能刚,等.含水室燃气-蒸汽弹射动力装置汽化机理研究[J].固体火箭技术,2018,41(06):792-798.
 HU Xiaolei,LI Rengfeng,XIE Nenggang,et al.Study on vaporization mechanism of gas-steam ejection power equipment containing water chamber[J].Journal of Solid Rocket Technology,2018,41(06):792-798.
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含水室燃气-蒸汽弹射动力装置汽化机理研究

参考文献/References:

[1]Eduist C T.Prediction of the launch pulse for gas generator launched missiles[R].AIAA 88-3290.

[2]Weiland C J,Vlachos P P,Yagla J J.Concept analysis and laboratory observations on a water piercing missile launcher[J].Ocean Engineering,2010,37(11):959-965.
[3]LIU Yongquan,Xi Anmin.An interior trajectory simulation of the gassteam missile ejection[J].Journal of Computers,2013,8(5):1321-1326.[4]Edquist C T,Rommin G L.Canister gas dynamics of gas generator launched missiles[R].AIAA 80-1186.
[5]袁曾凤.弹射内弹道中的相似方法研究[J].兵工学报,1987,8(1):8-18.YUAN Zengfeng.Simitude method in the interiorballistics of ejectors[J].Acta Armamentar ii,1987,8(1):8-18.
[6]张士卫,刘浩,丁朝臣.基于组件的弹射内弹道建模技术[J].兵器装备工程学报,2016,37(8):15-19.ZHANG Shiwei,LIU Hao,DING Chaochen.Component-based simulation modeling tecchnology of ejecting interior ballistics[J].Journal of Ordnance Equipment Engineering,2016,37(8):15-19.
[7]倪火才.变深度发射和能量可调发射动力系统[J].舰载武器,1998,6(1):16-25.NI Huocai.Changeable depth launch and energy adjustable ejection power system[J].Shipborne Weapons,1998,6(1):16-25.
[8]赵世平,鲍福廷.燃气蒸汽式发射系统内弹道若干问题研究[J].固体火箭技术,2003,26(3):7-10.ZHAO Shiping,BAO Futing.Analysis of several coefficients of interior ballistic evaluation for gas and steam launching system[J].Journal of Solid Rocket Technology,2003,26(3):7-10.
[9]陈庆贵,齐强,王海洋,等.潜射导弹发射内弹道仿真研究[J].导弹与航天运载技术,2011(6):40-42.CHEN Guiqing,QI Qiang,WANG Haiyang et al.Launching interior ballistic simulation of submarine-launched missile[J].Missiles and Space Vehicles,2011(6):40-42.
[10]Datta A,Som S K.Numerical prediction of air core diameter,efficient of discharge and spray cone angle of a swirl pressure nozzle[J].International Journal of Heat and Fluid Flow,2000,21(4):412-419.
[11]HOU Yan,TAO Yujia,HUAI Xiulan,GUO Zhixiong.Numerical characterization of multinozzle spray cooling[J].Applied Thermal Engineering,2012,39:163-170.
[12]肖虎斌,赵世平.燃气蒸汽式发射动力装置复杂内流场数值模拟[J].固体火箭技术,2009,32(4):35-38.XIAO Hubin,ZHAO Shiping.Numerical simulation of the complex flow field in combustion gassteam launching system[J].Journal of Solid Rocket Technology,2009,32(4):35-38.
[13]芮守祯,邢玉明.几种导弹弹射动力系统内弹道性能比较[J].北京航空航天大学学报,2009,35(6):766-769.RUI Shouzhen,XING Yuming.Comparative studies of interior ballistic performance among several missile eject power systems[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(6):766-769.
[14]张江华,史琼艳.考虑汽化的喷嘴高温气体注水两相流动规律[J].航空动力学报,2017,32(7):1545-1553.ZHANG Jianghua,SHI Qiongyan.Regularity of twophase flow with vaporization produced by injecting water to the high temperature airflow for nozzle[J].Journal of Aerospace Power,2017,32(7):1545-1553.
[15]刘伯伟,姜毅.汽化效应对燃气蒸汽式弹射气液两相流场的影响[J].固体火箭技术,2014,37(2):156-160.LIU Bowei,JIANG Yi.Influence of vaporization effect on gas-liquid two-phase flow field of ejection in combustion gas and vapor model[J].Journal of Solid Rocket Technology,2014,37(2):156-160.[16]李仁凤,乐贵高,马大为,等.结构参数对燃气蒸汽弹射载荷和弹道影响[J].上海交通大学学报,2016,50(11):1789-1794.LI Renfeng,LE Guigao,MA Dawei,et al.Effectof structural parameters on gas-steam ejection power system[J].Journal of Shanghai Jiaotong University,2016,50(11):1789-1794.?
[17]胡晓磊,乐贵高,马大为,等.水下燃气蒸汽弹射气液两相流场数值研究[J].航空动力学报, 2015,30(1):164-172.HU Xiaolei,LE Guigao,MA Dawei,et al.Numerical study of gas-steam ejection gas-liquid two-phase flow field under water[J].Journal of Aerospace Power,2015,30(1):164-172.
[18]郝继光,姜毅,韩书永,等.一种新的动网格更新技术及其应用[J].弹道学报,2007,19(2):88-92.HAO Jiguang,JIANG Yi,HAN Shuyong,et al.A new dynamic mesh update method and its applications[J].Journal of Ballistics,2007,19(2):88-92.
[19]SHI T H.A new k Eddy viscosity model for high Reynolds number turbulent flows-model development and validation[J].Computers & Fluids,1995,24(3):227-238.
[20]郭佳肄,胡晓磊,孙船斌,等.开口向上的环形腔宽度对弹射载荷的影响[J].兵器装备工程学报,2016,37(12):42-44.GUO Jiayi,HU Xiaolei,SUN Chuanbin,et al.Chamber width Influence on gas-ejection load[J].Journal of Ordnance Equipment Engineering,2016,37(12):42-44.[21]JIANG Yi,MA Yanli,WANG Weichen,et al.Inhibition effect of water injection on afterburning of rocket motor exhaust plume[J].Chinese Journal of Aeronautics,2010,23(6):653-656.

更新日期/Last Update: 2019-01-03
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