turbojet engine
涡轮式喷射引擎;[航] 涡轮喷气发动机;喷气涡轮机
2025-01-06 21:26 浏览次数 1
涡轮式喷射引擎;[航] 涡轮喷气发动机;喷气涡轮机
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。
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。
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。
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 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。
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蹤进行了仿真验证。
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。
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。
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。
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。
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。
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。
stimulation to the pilotless aircraft turbojet engine proves several advantages of this controlling method, such as good robustness, sensitive response, and minimal stable error.
对某型无人机涡喷发动机控制系统的仿真结果表明此控制方式具有鲁棒性好、响应速度快、稳态误差小等优点。
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。
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;
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。