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Thermal Stress Analysis

Often an object will fail because of stresses induced by uneven heating, rapid temperature change or differences in thermal properties. A coupled analysis, which models both thermal and stress variations, can be effective in predicting the overall structural response. It facilitates effective prediction of incidents where thermal expansion is an important consideration, such as in reciprocating & gas turbine engine design.

The usual procedure is to carry out a thermal analysis which evaluates the temperature distribution. These temperatures can then be used to prime the displacement analysis, and hence thermal deflections, strains & stresses can be evaluated.

It is also possible to have fully coupled analyses where the temperatures & displacements are a function of each other. This is most evident in analyses that involve fluid flows, such as in a gas turbine or rocket. The heat transfer rates are dependent on mass flow rates, but mass flow rates are a function of valve & seal clearances (labrynth seals in gas turbines, nozzles in rockets). Therefore, we end up with a scenario where clearances are a function of temperature and temperature is a function of clearances. This type of problem can only be solved via a non-linear and fully coupled solution.

 

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Thermal stress

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