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

[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.

[发布机构] A. Ishlinsky Institute for Problems in Mechanics, Russian Academy of Sciences, Vernadsky prospect 101(1), Moscow; 119526, Russia^1

[效力级别] 力学 [学科分类] 力学，机械学

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