comsol - tomasz strek home page
comsol - tomasz strek home page
comsol - tomasz strek home page
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Highlights 2010<br />
A stator blade in the turbine stage of a jet engine is<br />
heated by the combustion gases. To prevent the stator<br />
from melting, air is passed through a cooling duct in<br />
the blade. The resulting temperature gradients introduce<br />
significant stresses. Shown is the temperature<br />
distribution throughout the blade, as well as the von<br />
Mises stresses in both welds.<br />
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Intro<br />
Cov ToC + – A<br />
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