Digital simulation of gas turbine engine performance is a means to estimate all the engine performance parameters at the design point to a more accurate extent. This is an easy approach to simulate the complex gas turbine engine, and it can also be regarded as foundation on which the complicated off-design-point analysis is based. The present work is based on numerical analysis by digital computer, assuming quasi-one-dimensional flowfield and the gas mixture obtained from the combustion of air and fuel (CHx) as the working fluid. The thermodynamic properties of this gas mixture is assumed to be continuous functions of temperature and fuel-air ratio. Simulation of the turbojet engine, separated flow turbofan engine, mixed flow turbofan engine, and turbojet engine and turbofan engine with afterburner is carried out.
|頁（從 - 到）||319-328|
|期刊||Chung-Kuo Chi Hsueh Kung Ch'eng Hsueh Pao/Journal of the Chinese Society of Mechanical Engineers|
|出版狀態||Published - 1986 十月 1|
All Science Journal Classification (ASJC) codes