Effect of the stagnation temperature on the normal shock wave

DOI10.3233/JCM-2009-0253zbMATH Open1179.80037OpenAlexW2036529567WikidataQ127987187 ScholiaQ127987187MaRDI QIDQ3181674

Toufik Zebbiche

Publication date: 12 October 2009

Published in: Journal of Computational Methods in Sciences and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.3233/jcm-2009-0253

zbMATH Keywords

entropyinterpolationsupersonic flownormal shock waverelative errorsubsonic flowsupersonic nozzlehigh temperaturethermodynamics ratios

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20)

Related Items (1)

Gas effect for oblique and conical shock waves at high temperature

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