Basing on numerical optimization principles and thermodynamic performance design, efforts were made to optimize the design of finned-tube lubricate heat exchangers used in helicopters.
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释义
摘要在直升机肋管式滑油换热器的初步热力性能设计计算基础上,应用数值优化原理,对滑油换热器结构的优化设计进行了研究,建立了结构优化程序。
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