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模拟冲压进气条件对PDE推力测量影响
引用本文:范育新,王家骅,曹梦源.模拟冲压进气条件对PDE推力测量影响[J].推进技术,2008,29(2):225-229.
作者姓名:范育新  王家骅  曹梦源
作者单位:南京航空航天大学,能源与动力学院,江苏,南京,210016
摘    要:研究了射流模拟冲压进气条件下,气源喷口尺寸和气源压头对脉冲爆震发动机(PDE)地面台架试验推力测量的影响,分析地面台架试验中阻力和测量推力随模拟进气条件变化的规律。研究结果表明,PDE充填速度随气源压头或气源喷口尺寸的增加而增加;PDE阻力随气源压头的增加线性增加,随喷口尺寸增加而增加;喷口尺寸在78~105 mm内,PDE台架测量推力随喷口尺寸增加而增加。

关 键 词:脉冲爆震发动机  射流  推力  阻力
文章编号:1001-4055(2008)02-0225-05
修稿时间:2007年1月17日

Influence of simulative flight condition on thrust measurement of pulse detonation engine
FAN Yu-xin,WANG Jia-hua and CAO Meng-yuan.Influence of simulative flight condition on thrust measurement of pulse detonation engine[J].Journal of Propulsion Technology,2008,29(2):225-229.
Authors:FAN Yu-xin  WANG Jia-hua and CAO Meng-yuan
Institution:(Coll.of Energy and Power,Nanjing Uni.of Aeronautics and Astronautics,Nanjing 210016,China)
Abstract:Influence of nozzle size and the jet flow dynamic pressure at nozzel exit under simulative flight condition on test bench thrust value of pulse detonation engine was studied.Variation law of test bench resistance along with diversification simulative flight condition was analyzed.It showed that the filling velocity and resistance of PDE increasing with nozzle size and flow dynamic pressure at nozzel exit,and resistance increasing linearly with flow dynamic pressure.Thus test bench thrust increased with nozzle size in the range from 78 to 105 mm.
Keywords:Pulse detonation engine(PDE)  Jet flow  Thrust  Drag
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