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返回舱自由振动跨声速非定常流场数值模拟
引用本文:周伟江.返回舱自由振动跨声速非定常流场数值模拟[J].空气动力学学报,2000,18(1):46-51.
作者姓名:周伟江
作者单位:北京空气动力研究所,北京,100074
摘    要:本文利用NND差分格式对返回舱俯仰运动和跨声速绕流流场进行了耦合求解,结果表明来流M

关 键 词:跨声速流  非定常流  数值模拟  返回舱  自由振动
文章编号:0258-1825(2000)01-0046-06
修稿时间:1998-08-27

Numerical Simulation of Unsteady Transonic Flow around a Free Oscillating Reentry Vehicle
Zhou Weijiang.Numerical Simulation of Unsteady Transonic Flow around a Free Oscillating Reentry Vehicle[J].Acta Aerodynamica Sinica,2000,18(1):46-51.
Authors:Zhou Weijiang
Institution:Zhou Weijiang; (Beijing Institute of Aerodynamics,Beijing
Abstract:The coupling solution of a transonic flow and a free oscillating reentry vehicle using numerical method is presented,the phenominon of equi amplitude pitching motion of reentry vehicle has been shown.The period of pitching motion is about 2.8 second,and the amplitude is about 6.0 degree.These results are almost same as that obtained in flight experiment and wind tunnel test.
Keywords:transonic flow  unsteady flow  numerical simulation
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