二维带动力吸气式高超声速飞行器绕流的PNS-NS混合求解
PNS-NS combined method for solving two-dimensional powered airbreathing hypersonic vehicle's flowfield
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摘要: 为了提高吸气式高超声速飞行器绕流的求解效率,采用空间推进求解抛物化PNS(parabolizedNavier-Stokes)方程和时间迭代求解Navier-Stokes(N-S)方程的混合计算流体动力学(CFD)方法来求解高超声速飞行器整机绕流.在超声速占主导的流动区域采用空间推进求解抛物化N-S方程的方法,在亚声速和分离区采用时间迭代求解N-S方程的方法.对于求解二维带化学反应的吸气式高超声速飞行器绕流,混合CFD方法和完全时间迭代方法相比,可得到同等准确的数值模拟结果,并且求解效率提高了数倍.
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关键词:
- 吸气式高超声速飞行器 /
- 化学反应流动 /
- 抛物化Navier-Stokes方程 /
- 空间推进方法 /
- 混合计算流体动力学方法
Abstract: To improve the computational efficiency of airbreathing hypersonic vehicle's flowfield,a combined computational fluid dynamics(CFD) method,which combines space marching method for parabolized Navier-Stokes(PNS) equations and time iteration method for Navier-Stokes(N-S) equations,was used to simulate airbreathing hypersonic vehicle's flowfield.Space marching method was used to solve the PNS equations in the supersonic dominated regions,and time iteration method used to solve the N-S equations in the stream direction separation or subsonic dominated regions.For solving the two-dimensional(2-D) airbreathing hypersonic vehicle's flow field with chemical reaction,the combined CFD procedure can get the same results with the same accuracy and also improve computational efficiency for several folds as compared with traditional time iteration methods.
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