Performance Calculation Of Uniaxial Turbofan Engine

Performance calculate of aero engine has been a very important technology in its research, design, manufacture, experiment and application. In choosing and optimizing the cycle parameter, designing control rule and flow, simulating the impetus system and integrative design of the aircraft and aero engine, it is also the basic element.The uniaxial turbofan engine has the characteristic of low cost, low fuel consuming. It will be used in one-off tactics-stratagem attack weapons and robot bomb broad. Making exploratory research on turbofan engine, brought forward the method of the calculating, solving the practical problem, all of the work will promote the design of turbofan engine to take much more possession of the market and promote the modernization of the national defense.The dissertation centralized discuss the usual calculate process of the internal-combustion engine, the co-working equation of the uniaxial fan engine to solve the problems of the uniaxial fan engine calculating and make an attempt to calculate a certain engine.