Turboprop Engine Performance Simulation and Analysis

摘要：

Due to mature technologies, high reliability, low fuel consumption as well as a substantial increase in oil prices, civil regional aircrafts powered by turboprop have always had a high degree of importance. With the rapid development of the computer technology, performance calculating of the aero engine has been a very important technology in its research, design, manufacture, experiment and application. Based on the research on the structure and working principle of turboprop engine, a numerical model of turboprop engine was presented after the detailed analysis on calculating methods of thermodynamic parameters and performance parameters. Developed with the programming language C+ +, the numerical simulation software was established.

关键词： turboprop engine (numerical simulation performance calculation thermodynamic cycle parameters

作者: WANG Xiao-rong WANG Zhan-xue LIU Zeng-wei

作者单位: School of Engine and Energy,Northwestern Polytechnical University,Xian,China

会议类型: 国际会议

会议名称: 4th International Symposium on Jet Propulsion and Power Engineering(第四届喷气推进与动力工程国际会议 ISJPPE2012)

会议地点: 西安

会议语种:英文

页码: 521-524

在线出版日期: 2012-09-10（万方平台首次上网日期，不代表论文的发表时间）