turbofan engine

1. Numerical Simulation Study of a Three-dimensional Unsteady Flow in a Fan Under Distorted Air Admission Conditions Investigation of disturbed board total pressure distortion on a certain turbofan engine
   畸变进气条件下风扇三维非定常流动数值模拟某型涡扇发动机扰流板进气总压畸变研究
2. Selection of reliability parameters and targets assessment for certain missile turbofan engine
   弹用涡扇发动机可靠性参数选择及评定方法
3. Aerodynamic stability assessment for compression component running in turbofan engine with distorted flow
   畸变进气时涡扇发动机整机环境下压缩部件气动稳定性评定
4. An algorithm is developed based on the N-R ( Newton-Raphson) iteration method to solve the nonlinear mathematical model of turbofan engine.
   提出一种基于N-R迭代方法的有限域优化搜索法，用于求解涡扇发动机数学模型。
5. As an example, the development of a high bypass ratio turbofan engine was used to demonstrate how the constraints restrict design cycle parameters.
   以发展大涵道比涡扇发动机为例，说明了约束条件对设计循环参数的限制。
6. Preliminary analysis of thermodynamic cycle of an intercooled recuperated turbofan engine
   中冷回热航空涡扇发动机热力循环初步分析
7. Ideal Starting Procedure Analysis and Optimization Control Investigation for Turbofan Engine
   涡扇发动机理想起动过程分析与控制问题探讨
8. 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.
   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。
9. A Digital Electronic Controller of A Certain Turbofan Engine
   某型涡扇发动机数字式综合电子调节器研制
10. In turbofan engine's design, the structure with a large meridional expansion was used between HP and LP turbine, and this structure has brought the difficulty for the low pressure turbine design.
    在涡扇发动机的设计中，高低压涡轮过渡段处多采用较大子午扩张的结构，此结构给低压涡轮设计带来了难度。
11. Dynamic acceleration process identification for turbofan engine using Volterra-Laguerre expansion model
    基于Volterra-Laguerre扩展模型的发动机加速过程辨识
12. Self-Adaptation Simulation of Turbofan Engine Based on Components Characteristics
    基于部件特性自适应的涡扇发动机仿真
13. This report discusses the study of detailed nonlinear real time performance simulation for a two spool turbofan engine with afterburner.
    本文就双轴加力涡扇发动机详细非线性实时仿真模型进行了研究。
14. Research on turbofan engine HP-compressor rotor-12 blade tip clearance control
    某型发动机高压12级转子叶尖间隙控制研究
15. Analysis of Key Technologies of Turbine Structural Design for High Bypass Ratio Turbofan Engine
    大涵道比涡扇发动机涡轮结构设计关键技术分析
16. The development and design features of the high bypass ratio turbofan engine in foreign are comprehensively summarized.
    较为系统地总结了国外大涵道比涡扇发动机的研制特点和设计特点。
17. An Experimental Study on EEC Dynamic Model of a Turbofan Engine
    某涡扇发动机综合电子调节器动态模型试验研究
18. Experiments on infrared radiation characteristics of exhaust system for a turbofan engine
    某型涡扇排气系统缩比模型红外辐射特性实验
19. Power extraction method for acceleration and deceleration control law design of turbofan engine
    涡扇发动机加减速控制规律设计的功率提取法
20. Preliminary Concept of More Electrical Technology Based on Turbofan Engine
    基于涡扇发动机的多电技术研究初步设想
21. Based on the configuration of turbofan engine and combining the concept of variable cycle engines, the collectivity configuration of variable cycle engine is analyzed.
    基于涡扇发动机的结构平台，围绕变循环概念，分析了变循环发动机的原理与结构。
22. A Simulation System of Turbofan Engine Based on Virtual Reality
    基于虚拟现实技术的航空涡扇发动机仿真系统
23. Multiple Turbine Inter-stage Burners Turbofan Engine Performance Research
    多级涡轮级间燃烧室发动机与常规涡轮喷气发动机性能对比研究
24. This method has been successfully applied to a turbofan engine and the simulation results show the feasibility and effectiveness of the proposed method.
    本文将此方法成功应用于某涡扇发动机，取得了良好的效果，验证了本方法的可行性。
25. It means that the effects of Reynolds number must be taken into account in turbofan engine performance simulation at high altitude with low flight speed.
    因此在高空低速区航空发动机性能数值模拟必须考虑部件特性雷诺数的影响。
26. And then taking a dual-shaft turbofan engine as an example, numerical experiments were conducted for noise and results analysis. Finally, the development of the system was discussed.
    然后以一个双轴分排涡扇发动机为例，针对气路部件故障诊断和优化调整给出了考虑噪声的数值试验分析。最后就该系统的发展进行了讨论。
27. Performance Deterioration and Control of Military Turbofan Engine
    军用航空涡扇发动机性能衰减及控制
28. An Effective Measure of Enlargement Airstart Envelope for Turbofan Engine& Summary of Assisted Airstart for Aeroengine Starter
    1项扩大涡扇发动机空中起动包线的有效措施&浅论航空发动机起动机辅助空中起动
29. Simulation of Optimization of Variable Geometry for a Turbofan Engine of a Missile
    弹用发动机多变量组合调节优化仿真研究
30. Computation and assessment of aerodynamic stability of turbofan engine for missile
    弹用涡扇发动机气动稳定性计算与评定

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 engineturbojetturbojet engineturbofan