Analyse the traveling wave induction launcher temperature field with the method of ANSYS electromagnetic analysis (thermal coupling module).
用ANSYS分析电磁——热耦合的方法，分析了行波发射器的温度场。
The algorithm about the governing equation, boundary conditions under such transformation are also presented, which will be the basis for the calculation of coupling fluid field with thermal response.
给出了有关控制方程、边界条件的处理方法，为进一步耦合计算提供了有关基础。
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