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Analysis on Hypersonic Unsteady Aerodynamics and Dynamic Performance of an Lifting Body Hypersonic Vehicle

机译:升降式高超声速飞行器高超声速非定常空气动力学和动力性能分析

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The purpose of this paper is to simulate the unsteady aerodynamics andrnflight dynamic of an lifting body hypersonic vehicle at hypersonic conditions. Thernflow simulation use an advanced structured time-accurate Navier-Stokes equation.rnDual time-step approach in conjunction with LU-SGS implicit method was utilized.rnRoe scheme which was in combine with stiff moving grid generation technologyrnwas used for spatial discretization. The CFD/RBD coupling algorithms setup thernfoundation for vehicle dynamic aerodynamic analysis and virtual flight simulation.rnFrom the aerodynamic and flight dynamic results, the dynamic stability of thernvehicle have been studied.
机译:本文的目的是模拟高超声速条件下举升体高超声速飞行器的非定常空气动力学和飞行动力学。流动仿真使用先进的结构化时间精确的Navier-Stokes方程。rnDual时间步长方法与LU-SGS隐式方法结合使用。rnRoe方案与刚性移动网格生成技术结合使用,用于空间离散化。 CFD / RBD耦合算法为车辆动态空气动力学分析和虚拟飞行仿真奠定了基础。从空气动力学和飞行动力学结果出发,研究了车辆的动态稳定性。

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