以下为句子列表：
英文: By using the method of aircraft and turbofan engine integrated analysis, a model of maneuverable missile and turbofan engine integrated constrain analysis and mission analysis was developed and the computative examples and the analysis were given.
中文: 摘要利用飞机／涡扇发动机一体化设计的思路，建立了飞航导弹／涡扇发动机一体化设计的约束分析和任务分析模型并给出了算例和分析。
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英文: The mission section, the constrain conditions, the weight composition of the maneuverable missile, and the model of used in turbofan engine maneuverable missile were presented.
中文: 简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。
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英文: The relevance functions between total pressure recover coefficient and the parameters (Mach number, angle of attack, flow coefficient, angle of sideslip) for subsonic submerged inlet in turbojet and turbofan engine were investigated.
中文: 摘要根据某埋入式进气道试验数据建立了计算埋入式亚声速进气道总压恢复系数的经验公式，表现为关于马赫数、流量系数、攻角、侧滑角的函数。
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英文: This experiential formula can be used in simulating steady condition, startup, acceleration work process and integrated design of cruise missile and turbofan engine so as to improve the accuracy of 1D engine performance computation.
中文: 该经验公式可用于弹用发动机稳态、起动、加速过程的计算和导弹与发动机一体化设计的数值仿真模型，从而提高发动机性能数值仿真的准确性。
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