通过分析给定热源条件下的机舱内温度场,为加热器位置的布置、机舱内零部件保温提供参考。
Temperature and flow field inner the nacelle are calculated and analyzed, the results and conclusion could be used as reference for design of wind turbine nacelle.
通过分析给定热源条件下的机舱内温度场,为加热器位置的布置、机舱内零部件保温提供参考。
Temperature and flow field inner the nacelle are calculated and analyzed, the results and conclusion could be used as reference for design of wind turbine nacelle.
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