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逆流矢量喷管流动自身导致的非定常现象
引用本文:汪明生,杨建军.逆流矢量喷管流动自身导致的非定常现象[J].航空学报,2009,30(4):630-636.
作者姓名:汪明生  杨建军
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: 基于数值方法,研究了逆流推力矢量喷管中由于流动自身导致的非定常现象。结果表明,当抽吸背压下降至某个范围时(50.66~60.8 kPa),主流在接近外套壁面的某个位置处呈现出周期性振荡,流动参数(抽吸二次流量、推力矢量角、合成推力系数)也以小振幅振荡,但是同向二次流量却没有振荡。深入的流动机理分析表明,此时在逆流剪切层中,分离涡周期性地形成和发展,没有呈现出流动失稳,同时剪切层中的速度比又远大于定常流动下的值,因此流动表现为自激振荡特征。

关 键 词:射流推力矢量  逆流矢量喷管  数值模拟  非定常流动  主流附体  

Flow-induced Unsteady Phenomena in Counterflow Vectoring Nozzles
Wang Mingsheng,Yang Jianjun.Flow-induced Unsteady Phenomena in Counterflow Vectoring Nozzles[J].Acta Aeronautica et Astronautica Sinica,2009,30(4):630-636.
Authors:Wang Mingsheng  Yang Jianjun
Institution:College of Energy and Power Engineering;Nanjing University of Aeronautics and Astronautics;Nanjing 210016;China
Abstract:Unsteady phenomena induced in a counterflow vectoring thrust nozzle by the flow itself are studied by numerical simulation. The results show that when suction back pressure drops to a certain range (about 50.66-60.80 kPa), the main flow oscillates periodically at a location near the collar, and flow parameters (suction flow mass, vectoring angle and synthesis thrust coefficient) also oscillate periodically at a small amplitude, but the coflow keeps stable. This indicates that it is the counterflow shear lay...
Keywords:fluidic vectoring thrust  counterflow vectoring nozzle  numerical simulation  unsteady flow  main flow attachment  
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