@inproceedings{c2474e7b9659434e8bb7fe44a0020a68,
title = "Parametric analysis for intercooled recuperated turbofan engines",
abstract = "This paper aims at delivering a good insight into Intercooled Recuperative Engine Cycle through parametric analysis. Firstly, a numerical simulation model is created for an intercooled recuperated tri-spool turbofan engine with split exhaust. Secondly, aided by this model, couple relationships are analyzed between the IRA engine design parameters, heat exchanger design parameters, engine performance, and heat exchanger weight. Results show that; (1)The optimal overall pressure ratio for inter-cooled recuperated cycle engine decreases with the increase of heat exchanger efficiency; (2)Design aspects such as the mass flow ratio, the pressure ratio split between intermediate and high pressure compressor are found to greatly affect the perform-ance of the proposed IRA engine. (3)The higher the effectiveness of the recuperator effectiveness, the lower the SFC and the optimum OPR is also lower. However, the weight penalty increased dramatically.",
keywords = "Intercooled Recuperative Engine Cycle, Intercooler, Recuperator, Thermal dynamic, Turbofan engine",
author = "Min Chen and Suming Luo and Mengyuan Cao and Hailong Tang",
year = "2010",
language = "英语",
series = "Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010",
publisher = "Northwestern Polytechnical University",
pages = "1056--1058",
booktitle = "Proceedings of 2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010",
address = "中国",
note = "2010 Asia-Pacific International Symposium on Aerospace Technology, APISAT 2010 ; Conference date: 13-09-2010 Through 15-09-2010",
}