Under the given structure andboundary conditions, the average total pressure loss within the back pressure segment is 0.14 MPa.
在给定的结构和边界条件下，回压段内的总压损失平均为 0.14 MPa。
参考来源 - 天然气跨音速气水分离过程中收敛According to the sample provided by uniform method,the compressive angles are chosen as design variables,and the drag coefficient,total pressure recovery coefficient,pressure rising ratio and the combination of these three variables are designed as optimization objects.
根据均匀分析提供的样本,选取气流折转角为设计变量,阻力系数、总压恢复系数、进气道升压比及三者的组合作为优化目标。
参考来源 - 基于混合遗传算法的进气道性能设计与优化 in C·2,447,543篇论文数据，部分数据来源于NoteExpress
以上来源于: WordNet
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