Three-Dimensional Calculation of Double Cone 25°/55° Aerothermodynamics Using a Family of Computer Codes UST3D

I. A. Koryukov, P. Silvestrov, D. V. Ishin
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Abstract

A numerical modeling of the three-dimensional flow around a 25°/55° double cone by a high-velocity gas flow on an unstructured grid is carried out. Numerical simulation was carried out in N2 (nitrogen) gas. For numerical simulation, the author's computer codes UST3D-AUSMUP2, UST3D-AUSMPW and USTFEN, developed at IPMech RAS, were used. These computer codes are based on the model of the complete system of Navier-Stokes equations for a perfect gas, which is solved by different methods on an unstructured grid. Validation and verification of the obtained results were carried out. For numerical simulation of the flow, a geometric model of a double cone 25°/55° was constructed.
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双锥25°/55°空气热力学的三维计算
对高速气流在非结构网格上绕25°/55°双锥的三维流动进行了数值模拟。在N2(氮气)气体中进行了数值模拟。数值模拟使用作者在IPMech RAS开发的计算机代码UST3D-AUSMUP2、UST3D-AUSMPW和USTFEN。这些计算机代码是基于完美气体的Navier-Stokes方程组的完整系统模型,在非结构化网格上用不同的方法求解。对所得结果进行了验证和验证。为了进行数值模拟,建立了25°/55°双锥的几何模型。
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