Mach number distribution for subsonic flow over a bump.

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Surface heat transfer coefficient for VKI MUR 241 Cascade.

Jiří FÜRST, Professor, Czech Technical University in Prague, Prague, ČVUT, Faculty of Mechanical Engineering (FS)

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Cross-sectional (x − y) views of the computational domain and the grid

Volume fraction contours once cavity fully developed.

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A physical explanation for the formation of shocks in transonic flow. ( Description in the comments) : r/TurbineEngines

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Mach number distribution for subsonic flow over a bump.

Pressure distribution over the test turbine blade, comparison with