Gas effect for oblique and conical shock waves at high temperature

DOI10.1051/MMNP/2020036zbMath1475.76057OpenAlexW3091752652MaRDI QIDQ5001348

Mohamed Boun-Jad, Abderrazak Allali, Toufik Zebbiche, Toufik Yahiaoui

Publication date: 19 July 2021

Published in: Mathematical Modelling of Natural Phenomena (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1051/mmnp/2020036

zbMATH Keywords

shock waveRunge-Kutta schemeshock reflectionaerodynamic coefficientdetonation propulsionintake adaptation

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Gas dynamics (general theory) (76N15) Diffusive and convective heat and mass transfer, heat flow (80A19)

Cites Work

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• Effect of the stagnation temperature on the normal shock wave
• A First Course in the Numerical Analysis of Differential Equations
• High-order Explicit Runge-Kutta Formulae, Their Uses, and Limitations
• Approximation for weak and strong oblique shock wave angles

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