Turbojet engines are older, simpler in design and ideal for high-speed, high-altitude flight; turbofan engines are more modern, featuring a fan for increased efficiency, making them suitable for commercial aviation.
1) turbojet/turbofan engine 涡喷/涡扇发动机 1. A computer program is developed to analyze the effects of circumferential inlet total-pressure distortion on the stability and performance parameters ofturbojet/turbofan engines. 开发了一种用于计算进气总压周向畸变对涡喷/涡扇发动机气动稳定性和主要性能参数...
Turbofan definition: a jet engine having a large impeller that takes in air, part of which is used in combustion of fuel, the remainder being mixed with the products of combustion to form a low-velocity exhaust jet.. See examples of TURBOFAN used in a se
Related to Turbofans:fanjet,Bypass ratio tur·bo·fan (tûr′bō-făn′) n. 1.A turbojet engine in which a fan supplements the total thrust by forcing air directly into the hot turbine exhaust. 2.An aircraft in which a turbofan is used. In both senses also calledfanjet. ...
Turbofan and Turbojet Gas Turbine Engine Test Cell Correlationdoi:SAE ARP741B本文描述了用于涡扇发动机和涡轮喷气发动机性能试验的试验室相关性的推荐规程和程序.测试单元相关性用于确定任何给定测试单元外壳和设备相对于发动机基准性能对发动机性能的影响.当在室内测试单元中进行基线测试时,基线性能数据将根据露天条件...
TR 900 Turbojet Turbofan Engine Model Brushless Motor Fan Electric Reverse Thrust Function PLA 3D Printing Process Toy Model Parameters Name: Turbofan engine model Material: PLA plastic Process: 3D printing Product status: finished product Product size: 25CM*10CM*12CM ...
Turbofan aero-engine description and performance measures Turbofan aero-engines comprise the most common propulsion system for modern era commercial and military aircraft, alternatively referred to as “bypass” engines. Unlike turbojet engines, which do not divert any portion of suctioned air mass, tu...
English Name: Measurement Method for Parameter of Turbojet Engine and Turbofan Engine for Missile - Thrust Chinese Name: 弹用涡轮喷气和涡轮风扇发动机参数测量方法 推力 Chinese Classification: V72 Spacecraft power system Professional Classification: QJ Professional Standard - Aerospace Issued on: 1994-...
A tip turbine engine according to the present invention includes a plurality of independently variable inlet guide vanes for the fan and/or for the compressor. An actuator is operat
However, the turbofan engine is a complex aerodynamic thermodynamic system with multi-variable, nonlinear, and time-varying characteristics, so the control-oriented modeling of the turbofan engine faces great challenges. The modeling needs to resolve the contradiction between model accuracy and real-time...