Improved Multiple Point Nonlinear Genetic Algorithm Based Performance Adaptation Using Least Square Method
Author:
Affiliation:
1. School of Engineering, Cranfield University, Cranfield, Bedford MK43 0AL, UK
2. China Aviation Powerplant Research Institute, Aviation Industry Corporation of China, Zhuzhou, Hunan Province, PC 412002, P.R. China
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4004395/5893140/031701_1.pdf
Reference16 articles.
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4. Component Map Generation of a Gas Turbine Using Genetic Algorithms;Kong;ASME Conf. Proc.
5. Components Map Generation of Gas Turbine Engine Using Genetic Algorithms and Engine Performance Deck Data;Kong;J. Eng. Gas Turbines Power
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