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fei ji ran you re fu he ji suan
Author(s): 
Pages: 34-38
Year: Issue:  2
Journal: Aircraft Design

Keyword:  超音速巡航燃油温度;
Abstract: 本文仅对飞机燃油系统燃油箱内的燃油温度计算,提出一套理论计算方法,利用该方法能够较准确计算飞机在超音速巡航时,燃油箱内燃油温度值。可节省更多的计算时间,提高燃油温度计算精确度。尤其是在燃油系统方案论证阶段,为燃油系统方案评审、决策提供理论依据。
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