System optimization of turbofan engines using genetic algorithms

A. Homaifar, H. Y. Lai, E. McCormick

研究成果: Article同行評審

29 引文 斯高帕斯(Scopus)

摘要

This paper presents an application of genetic algorithms to the system optimization of turbofan engines. Genetic algorithms are relatively new general-purpose optimization algorithms that apply the rules of natural genetics to explore a given search space. In order to characterize the many measures of aricraft engine performance, two different criteria are chosen for evaluation. These criteria are thrust per unit mass flow rate and overall efficiency. These criteria are optimized using four key parameters including Mach number, compressor pressure ratio, fan pressure ratio, and bypass ratio. After observing how each parameter influences objective functions independently, the two objective functions are combined to examine their interaction in a multiobjective function optimization. Numerical results indicate that genetic algorithms are capable of optimizing a complex system quickly. The resultant parameter values agree well with previous studies.

原文English
頁(從 - 到)72-83
頁數12
期刊Applied Mathematical Modelling
18
發行號2
DOIs
出版狀態Published - 1994 二月

All Science Journal Classification (ASJC) codes

  • 建模與模擬
  • 應用數學

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