Simulation of gas dynamics of hypersonic aircrafts with the use of model of high-temperature air and graphics processor units




waverider, hypersonic aerodynamics, physical and chemical processes, computational fluid dynamics, graphics processor unit, speed-up


Numerical simulation of the flow around a hypersonic aircraft is carried out using a high-temperature air model and a hybrid architecture based on high-performance graphics processing units. The calculations are performed with the Euler equations discretized by the finite volume method on unstructured meshes. The scalability of the developed implementations of the model is studied and the results of the study of the efficiency of calculating hypersonic gas flows on graphics processors are analyzed. The computational time spent with the perfect and real gas models is discussed.

Author Biographies

K.N. Volkov

D.F. Ustinov Baltic State Technical University «Voenmekh»,
Faculty of Rocket and Space Engineering
• Leading Researcher

Yu.V. Dobrov

A.G. Karpenko

S.I. Malkovsky

Computer Center of Far Eastern Branch of the Russian Academy of Sciences
• Researcher

A.A. Sorokin

Computer Center of Far Eastern Branch of the Russian Academy of Sciences
• Chief Researcher


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How to Cite

Волков К.Н., Добров Ю.В., Карпенко А.Г., Мальковский С.И., Сорокин А.А. Simulation of Gas Dynamics of Hypersonic Aircrafts With the Use of Model of High-Temperature Air and Graphics Processor Units // Numerical methods and programming. 2021. 22. 29-46. doi 10.26089/NumMet.v22r103



Methods and algorithms of computational mathematics and their applications

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