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交叉射流特性的试验研究 被引量:3

EXPERIMENTAL STUDY ON TURBULENT JET IN A CONFINED CROSSFLOW
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摘要 本文研究了稳燃腔中交叉射流两相流动。使用三维激光粒子动态分析仪 (PDA)测量了正三角形截面副射流与主射流速度比为 2 .5时的交叉射流流动 。 A turbulent triangular jet issuing perpendicularly into a confined gas particle two phase flow was investigated experimentally.When jet to crossflow velocity ratio R equaled to 2 5,mean and fluctuating velocity components were measured by the Three Dimensional Particle Dynamics Anemometry (3 D PDA).The PDA signals were evaluated to yield the turbulent intensity and the particle concentration.The measurement results show that the turbulent intensity in the wake of the crossflow is enhanced particularly on the edge of the recirculation zone.There are two particle concentration peaks,one of them is in the recirculation zone,and the other is on the edge of the zone.
出处 《航空动力学报》 EI CAS CSCD 北大核心 1993年第1期19-20,共2页 Journal of Aerospace Power
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参考文献1

  • 1徐明厚,工程热物理学报,1991年,13卷,1期

同被引文献23

  • 1周伟江,马汉东,李锋.超声速主流中横向喷流干扰流场数值模拟[J].航空动力学报,1993,8(1):6-10. 被引量:3
  • 2韩才元,华中理工大学学报,1991年,19卷,5期,84页
  • 3王应时,燃烧过程数值计算,1989年
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  • 6马明生,邓有奇,郑鸣,吴晓军.超声速侧向多喷流干扰特性数值模拟[J].空气动力学学报,2007,25(4):468-473. 被引量:9
  • 7Gnemmi P,Sch?fer H J.Experimental and numerical investigations of a transverse jet interaction on a missile body[R].AIAA-2005-52,2005.
  • 8Aswin G,Chakraborty D.Numerical simulation of transverse side jet interaction with supersonic free stream[J].Aerospace Science and Technology,2010,14(5):295-301.
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  • 10Srivastava B.Lateral jet control of a supersonic missile:computational and experimental comparisons[J].Journal of Spacecraft and Rockets,1998,35(2):140-146.

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