Numerical simulation of the flow over a hypersonic waverider using the method for splitting into physical processes

10th International Conference on Aerophysics and Physical Mechanics of Classical and Quantum Systems

物理学;力学

Yatsukhno, D.S.^1

A. Ishlinsky Institute for Problems in Mechanics, Russian Academy of Sciences, Vernadsky prospect 101(1), Moscow

119526, Russia^1

关键词: Aerodynamic characteristics;    Computational process;    Computer codes;    Physical process;    Unstructured grid;    Virtual modeling;    Waverider;   

Others  :  https://iopscience.iop.org/article/10.1088/1742-6596/815/1/012022/pdf
DOI  :  10.1088/1742-6596/815/1/012022

学科分类：力学，机械学

来源: IOP

【 摘 要 】

The aim of the study is to obtain hypersonic waverider aerodynamic characteristics over the angle-of-attack range from 0° to 10° at Mach 4. The simplified virtual model of the waverider was designed. The Navier-Stokes equations solution was performed using computer code into which the method for splitting into physical processes was implemented. The unstructured grid was used in the computational process.