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顺逆流向喷流干扰下二体分离气动力风洞实验研究及前体轴向力特性
引用本文:陈谟. 顺逆流向喷流干扰下二体分离气动力风洞实验研究及前体轴向力特性[J]. 宇航学报, 1995, 16(1): 46-52
作者姓名:陈谟
作者单位:北京空气动力研究所
摘    要:本文概述了具有顺,逆流向喷流干扰的二体分离气动力风洞实验技术研究。对有喷流干扰引起的前体轴向气动力特性,作了简单的介绍。最后对有顺、逆流向喷流干扰的前体底部流动模型作了定性的描绘,可供理论研究时参考。

关 键 词:风洞试验 喷流干扰 二体分离 气动特性

AN INVESTIGATION OF WIND-TUNNEL TEST TECHNIQUES OF TWO-BODIES SEPARATION WITH FLOW AND COUNTER FLOW DIRECTION JET INTERFERENCE AND FOR-BODY AXAIL FORCE CHARACTERISTICS
Chen Mo. AN INVESTIGATION OF WIND-TUNNEL TEST TECHNIQUES OF TWO-BODIES SEPARATION WITH FLOW AND COUNTER FLOW DIRECTION JET INTERFERENCE AND FOR-BODY AXAIL FORCE CHARACTERISTICS[J]. Journal of Astronautics, 1995, 16(1): 46-52
Authors:Chen Mo
Affiliation:Beijing Institute of Aerodynamics
Abstract:The paper describes an investigation of wind tunnel test techniques of two bodies separation with flow and counter flow diraction. jet Interference,and simply indroduces for-body axail force characteristics by induced jet.Finally, the report qualitatively dipcts the for-body base flow model with flow andcounter flow direction jet interence which can be used for theorytical reaserch.
Keywords:With flow and counter flow direction jet interference.  Two-bodies separation  Aerodynamics simulation  Aerdynamics characteristics  Base drag  
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