turbojet engine

1. Airplane powered by a turbojet engine.
   由涡轮喷气发动机推动的飞机。
2. A stage by stage mathematical model of the compressor in a turbojet engine is developed based on the control volume theory.
   根据控制体理论，建立了涡喷发动机中压气机的逐级数学模型。
3. Experiments were performed to investigate surge problem of a single shaft axial flow turbojet engine during throttling.
   对某型单轴涡喷发动机节流过程中的喘振故障进行了试验研究。
4. The improved and modification designs were conducted for a turbojet engine.
   对某型涡轮喷气发动机进行了改进、改型设计。
5. A special instument is presented for monitoring the transient process in a turbojet engine, which is called "transient operating line indicator".
   本文提出了一种测量涡喷发动机过渡过程的专用仪器&涡喷发动机过渡工作线显示仪。
6. The response of turbojet engine to the turbulence-type of dynamic inlet total pressure distortion is discussed in this paper.
   本文介绍涡喷发动机对湍流型动态畸变的响应。
7. Under the identical regime and inlet flow conditions, the performance of the twin spool turbojet engine was simulated respectively by real time model and non real time model.
   该实时模型包括：线性化的压气机特性模型、简化的涡轮特性以及非线性方程组的降维处理。
8. An airplane with an external propeller that is driven by a turbojet engine.
   由涡轮螺桨发动机驱使的有额外推动器的飞机。
9. The validation of the method is demonstrated by the identification examples of turbojet engine.
   以涡喷发动机辨识算例证明了该方法的有效性。
10. The characteristics of low thrust turbojet engine with a simple control program were studied.
    研究了用于无人飞行器上使用的小推力级涡喷发动机在简单控制规律下的多种重要特性。
11. 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
12. The results are helpful for the turbine guide blade design of the turbojet engine.
    其结果为涡轮导向器叶片设计改进提供了依据。
13. Thermal effects on transient process of a turbojet engine
    热效应对涡喷发动机过渡过程的影响
14. 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
15. 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
16. A model for 100N class micro turbojet engine is established. Software and hardware system design of the controller is accomplished by using robust control algorithm.
    建立了100N推力级微小型涡喷发动机模型，应用鲁棒控制算法进行了控制器软、硬件系统开发设计；
17. The rocket sled test can imitate the dynamic conditions of missile launching, it is very important for missile turbojet engine design.
    火箭橇试验能够真实的模拟导弹发射条件，它对于弹用涡轮喷气发动机研究具有十分重要的意义。
18. The design and test results of the new type high-subsonic speed submerged and semi-submerged intakes for cruise missile propelled by a turbojet engine have been introduced.
    本文介绍了以涡轮喷气发动机为动力装置的飞航式战术导弹的一种新型高亚音速嵌入式、半嵌入式进气道的设计与试验研究结果。
19. The compressor's aerodynamic instability problem of a certain turbojet engine in the process of the throttling operation was experimentally studied.
    对某型涡喷发动机节流过程中压气机的气动不稳定问题进行了分析研究。
20. Installation Evaluation and Adjustment of Turbojet Engine Parameters
    涡轮喷气发动机参数的装机评价和调整
21. This paper presents the test plan, the results of the station parameters measurement for a typical turbojet engine and the analysis of measurement results.
    本文介绍了一典型的涡轮喷气发动机全流程参数测量的试验方案、测试结果及分析。
22. A design of a twin variable control system for Aero-turbojet engine
    航空涡轮喷气发动机双变量控制系统设计
23. A scheme of condition monitoring and main faults diagnosing system for a turbojet engine
    某型涡喷发动机状态监控与主要故障诊断系统方案
24. As an example, a robust control law is designed to the twin spool turbojet engine system using the given method. The result shows that the given method is feasible.
    文中以双转子涡喷发动机控制器设计为例，设计了基于LMI的鲁棒控制器，结果表明所给方法是可行的。
25. The rocket sled test was carried out for overall investigating the dynamic process of missile turbojet engine starting and accelerating.
    为了研究弹用涡轮喷气发动机动态启动加速过程，开展了发动机火箭橇试验研究。
26. 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
27. Secondly, the particular structural design characteristics of this micro-turbojet engine are analyzed.
    其次，又对这台发动机独有的结构特点进行了分析；
28. 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。
29. The process of loosing compressor aerodynamic stability in a turbojet engine was analyzed using the correlation integral method.
    对某涡喷发动机压气机的气动失稳过程进行了相关积分分析。
30. 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。

noun

1. a jet engine in which a fan driven by a turbine provides extra air to the burner and gives extra thrust

   Synonym:    fanjetfan-jetfanjet engineturbojetturbofanturbofan engine