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二元矢量喷管流场的N-S方程计算
引用本文:封建湖. 二元矢量喷管流场的N-S方程计算[J]. 航空动力学报, 1996, 11(3): 237-240,328
作者姓名:封建湖
作者单位:西北工业大学封建湖,西安市西北工业大学应用数学系
摘    要:对二元矢量喷管在不同工况下的流场进行了数值模拟。求解的控制方程为三维非定常N-S方程。空间方向用有限体积离散,时间方向用Runge-Kutta法推进。粘性项的计算上采用了一种有限体积框架下新的离散化方法。湍流模型采用了广泛使用的Baldwin-Lomax代数模型。计算表明,本文方法能准确地计算二元矢量喷管、非矢量喷管在设计与大设计落压比下的流场。

关 键 词:喷管  矢量场  数值计算
收稿时间:1995-09-01
修稿时间:1995-12-01

NAVIER-STOKES PREDICTIONS OF 2-D VECTORED NOZZLE FLOWS
Feng Jianhu. NAVIER-STOKES PREDICTIONS OF 2-D VECTORED NOZZLE FLOWS[J]. Journal of Aerospace Power, 1996, 11(3): 237-240,328
Authors:Feng Jianhu
Affiliation:Dept. of Applied Mathematics, Northwestern Polytechnical University, Xi'an 710072
Abstract:In this paper,the viscous flows in the two-dimensional vectored and unvectored nozzles are numerically simulated by three-dimensional time-dependent Navier-Stokes equations in conservation forms.Finite volume discretization is used in spatial form and Runge-Kutta method in time marching direction.A new viscous terms' discretization in the frame-work of the finite volume method is used which has the advantages of less operation counts and full conservation.A modified Baldwin-Lomax algebraic turbulent model and wall function law are also adopted in the prediction.Comparision of numerical predictions with experiments shows that the Navier-Stokes code can accurately predict the flow fields in the vectored and unvectored nozzle where the flow is predominantly two-dimensional at the designed nozzle pressure ratios or above.Discrepancies between predictions and experiment are found at lower nozzle pressure ratios where separation typically occurs in a large portion of the nozzle.
Keywords:Jet nozzles Vector fields Numerical computation
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