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。
An annular combustor with evaporation tubes was designed for certain micro-turbojet engine.
为某微型涡喷发动机设计了一个蒸发管环形燃烧室。
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。
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。
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。
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。
Many off-design condition phenomena of a turbojet engine are related with the variation of incidence angles at front and rear compressor stages.
涡轮喷气发动机非设计状态下的许多现象都与共同工作时压气机前后各级攻角的变化有关。
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。
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。
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。
Simulations on the nonlinear model of the twin spool turbojet engine aerothermodynamics are conducted to verify the disturbance rejection and tracking performance.
所述方法在某型双转子涡喷发动机气动热力学非线性模型上对抗干扰性和目标跟踪进行了仿真验证。
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。
A brief view and results of tests for the effects of the inlet total pressure distortion on the performance and the stability of a two-spool turbojet engine are presented.
介绍进气总压畸变对双轴涡喷发动机性能和稳定性影响的试验及其结果。
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。
This paper covers the designs of hardware in the Loop Simulation (HILS) testing of minitype turbojet engine digital control regulator, and hardware and software configurations.
介绍了某小型涡喷发动机数控调节器的半实物仿真试验系统的设计，以及软件和硬件的试验配置。
Rotor unbalancing is one of the main causes of vibration and noise in aero-engine, especially in micro-turbojet engine, which affects work performance and fatigue life directly.
航空发动机尤其是高速旋转的微型涡喷发动机，不平衡是造成转子振动过大以及产生噪音的主要原因之一，直接影响发动机的工作性能和使用寿命。
The stability, reliability and performance of two spool turbojet engine will be affected by the matching correlation between 1st and 2nd turbine nozzle areas and engine nozzle area.
在双轴式涡轮喷气发动机中，及级涡轮导向器面积和尾喷口面积匹配关系影响到发动机工作稳定性、可靠性和性能。
As an example, the method provided was adopted to rectify the parameters in the simulation model of a given twin-spool reheated turbojet engine, and the simulation achieved satisfactory accuracy.
应用本文方法对某型双转子加力涡喷发动机仿真模型进行校正，获得了满意的仿真精度。
Taking the certain small scaled turbojet as an example, the influence by mass injection and pre-cooled engine was calculated and analyzed along fly trajectory.
并以某小型涡喷发动机为例，沿飞行轨迹计算分析了射流预冷却对发动机性能的影响。
This is the important research problem for starting of the jet engine in the sky. But it was researched for starting test of the small turbojet in the sky.
喷气发动机的空中起动是重要的研究课题，而小涡喷发动机的空中起动试验尚需探索。
This is the important research problem for starting of the jet engine in the sky. But it was researched for starting test of the small turbojet in the sky.
喷气发动机的空中起动是重要的研究课题，而小涡喷发动机的空中起动试验尚需探索。
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