turbojet engine的例句大全

The design criteria of engine anti-surge control system are concluded by means of tests and data analysis. The validity of the design criteria has been demonstrated by the development and flight test of a turbojet engine anti-surge control system.

通过试验和数据分析，得出了发动机防喘控制系统的有效性评价准则，而某型发动机防喘控制系统的研制和飞行试验证明了该有效性评价准则的正确性。

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Investigation of rocket sled test for missile turbojet engine

弹用涡轮喷气发动机火箭橇试验研究

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A Testing Instrument for the Box Against Pant of Some Turbojet Engine

某涡喷发动机防喘盒检测仪的研制

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Mathematical model and digital simulation for speed control system of two-spool turbojet engine

双转子涡轮喷气发动机转速控制系统数字仿真

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An analytical study of component matching regularity of turbojet engine

涡轮喷气发动机共同工作规律解析分析

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Research on characteristics of turbojet engine with simple control program

简单控制规律下涡喷发动机特性的研究

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Application of simulation model of sensors to analysis fault of control system of turbojet engine

应用传感器仿真模型分析发动机控制系统故障

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Design for scheme of reliability growth testing of turbojet engine

涡喷发动机可靠性增长试验方案的设计

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Analysis on Methods of Missile Turbojet Engine Condition Monitoring

弹用涡喷发动机的状态监控方法分析

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Performance monitoring and diagnosis system for missile turbojet engine

弹用涡喷发动机性能监视与诊断系统软件研制

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An Analysis of Noise Characteristics of a Turbojet Engine

某型涡轮喷气发动机噪声特性分析

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Experimental research on the simulation of distortion flow field for turbojet engine distortion test

涡轮喷气发动机抗畸变流场模拟试验研究

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Study on the Method Establishing the Revolution Difference Map for a Two-Spool-Turbojet Engine

双轴式涡喷发动机的转差线图确定方法的研究

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It was powered by an Allison J 33 A turbojet engine.

它由一阿利森J33座,阿涡喷发动机.

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A turbojet engine used to drive an external propeller.

由涡轮喷气发动机推动的飞机.

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The flight test of twin-spool turbojet engine simulating the ingestion of missile exhaust

双转子涡喷发动机吞吸导弹喷流飞行模拟试验

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The Temperature Distortion Generator ( TDG) design specifications, design technique and the technology of its fabrication were presented. The TDG was tested and calibrated using a turbojet engine and a turbofan engine.

介绍了航空发动机温度畸变试验装置设计技术与研制方法，主要设备及设计技术指标，以及用A型涡轮喷气发动机B型涡轮风扇发动机调试和对比试验结果。

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Turbojet engine is selected as propulsion system according to the practical situation.

从实际情况考虑选用涡轮喷气发动机。

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μ synthesis control with robust performance for missile turbojet engine

弹用涡喷发动机鲁棒性能μ综合控制

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Starting and accelerating model of missile turbojet engine in flight test

弹用涡喷发动机飞行试验启动加速性能仿真

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