加力涡扇发动机

加力涡扇发动机过失速/旋转失速特性分析

Modeling the rotating behavior of an augmented turbofan engine

无加力涡扇发动机二元喷管的红外辐射特性实验

An experimental investigation on infrared radiation characteristics of 2-D nozzles of turbofan engine afterburner

高性能加力涡扇发动机节流比对飞机性能的影响

The Impact of Throttle Ratio of Hign Performance Turbofan Engine with an Afterburner on Airplane Performance

军用加力涡扇发动机的设计

Design of Military Turbofan 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。

This report discusses the study of detailed nonlinear real time performance simulation for a two spool turbofan engine with afterburner .

对飞行模拟机用的多变量控制的双轴加力涡扇发动机实时性能仿真模型进行了研究。

Study of real-time performance simulation of a mixed-flow two-spool augmented turbofan engine used in a flight simulator was carried out .

强调论述了高性能加力涡扇发动机设计论证阶段的个重要概念节流比。

An important concept on the phase of high performance military turbofan engine 's designing , throttle ratio , is discussed in this paper .

为说明所建立的起动性能模型的模拟效果，将程序计算结果与试验结果进行了比较，结果表明该起动仿真模型能较准确地模拟混排加力涡扇发动机的地面起动过程。

In order to show the effect of the simulation , the results of the simulation model calculated have been compared with the testing results . The compared result shows that the simulation model can simulate mixed flow turbofan engine with afterburner for ground starting effectively .