turbofan的例句大全

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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[ 3]. The paper also points out that the inlet temperature of the turbofan after& burner is low and the temperature exponent of the stability parameter may be smaller than 1.

本文还指出涡轮风扇加力室进口温度低，稳定准则中的温度指数可能小于1。

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The results show that a turbofan engine with a small bypass ratio must be installed, and a suitable turbine entry temperature is obtained by optimization with life cycle cost.

结果表明宜采用小涵道比涡扇发动机，而且不考虑费用时涡轮前温度取值越高越好，考虑费用时则有最大值；

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Aerodynamic design characteristic of test cell for-high. by-pass ratio turbofan engine

大函道比涡扇发动机试车台气动力设计的特点

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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

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Also, problems shown at low-altitude(≤ 2km) simulation were pointed out from the characteristics of altitude simulation test for turbofan engines. Technology improvement was proposed.

并根据涡轮风扇发动机高空模拟试验的特点，指出了SB101高空台对涡轮风扇发动机进行低空（≤km）模拟中存在的问题，对存在的问题提出了技术改造方案。

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A method," gross thrust model", is developed to determine gross thrust of jet engine and afterburning turbofan engine in flight testing.

提出了一种飞机飞行中发动机推力测定的总推力模型。

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Research of Turbofan Engine Transient Process with Thrust Vectoring Nozzle

带矢量喷管的涡扇发动机动态过程研究

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Based on these two real time models, the real time mathematical model of the turbofan engine with thrust vectoring nozzle was acquired.

在以上两个模型的基础上建立了带轴对称矢量喷管的涡扇发动机数学模型。

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The Effect of Thrust Vector Control on the Performance of Turbofan Engine

矢量喷管控制对发动机性能的影响

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Performance optimization of high thrust-weight ratio turbofan engine

高推重比涡扇发动机性能寻优分析研究

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Numerical Simulation of the Influence of Nozzle Area Control Accuracy on Turbofan Afterburning Performance

喷管面积调节精度对某型涡扇发动机加力性能影响的数值仿真

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Aerothermodynamic Model of Turbofan Engine With Matlab Description

涡扇发动机气动热力模型的Matlab表达

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The Strength Design System of the Turbojet and Turbofan Engine

航空涡喷、涡扇发动机强度设计系统

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Key Technology of Modern High Bypass Ratio Turbofan Engine

现代高涵道比涡扇发动机关键技术

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A design method of QFT robust controller for the turbofan engine based on the Diagonal Dominance Precompensation using the theory of linear matrix inequalities ( LMI) is presented in this thesis.

论文提出了一种基于LMI对角占优预补偿的航空发动机多变量控制系统QFT鲁棒控制器设计方法。

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Analysis of turbojet and turbofan jet noise in aero engine test

涡喷、涡扇发动机试车台噪声分析

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Analysis of Some Typical Faults of Hydraulic System of Turbofan Jet Fuel-supplying Governing System

发动机供油调节器液压系统典型故障分析

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In this paper, damage tolerance characteristics are studied by experiment and theory analysis based on the wing beam integrated structure of the new turbofan jet airplane.

本文立足于工程实际，针对某民用支线飞机整体翼梁结构，通过试验和理论计算分析，研究了其损伤容限特性。

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Stability Assessment Test Technology of a Turbofan Engine Inlet Temperature Distortion

某型涡扇发动机进口温度畸变的稳定性评定试验技术研究

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