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Output details

12 - Aeronautical, Mechanical, Chemical and Manufacturing Engineering

Cranfield University

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Article title

Nonlinear Multiple Points Gas Turbine Off-Design Performance Adaptation Using a Genetic Algorithm

Type
D - Journal article
Title of journal
Journal of Engineering for Gas Turbines and Power : Transactions of ASME
Article number
-
Volume number
133
Issue number
7
First page of article
71701
ISSN of journal
0742-4795
Year of publication
2011
URL
-
Number of additional authors
5
Additional information

The research described in this paper was initially presented at the ASME Turbo Expo 2010 conference, where it won Best Paper Award in the Cycle Innovations Committee for that year. The developed new method was part of the delivery of the collaboration with China Powerplant Research Institute (CAPI) of Aviation Corporation Industry of China (AVIC) and is used by CAPI as part of their helicopter engine diagnostic system. CAPI Contact Mr Weimin Liu, 608.capi@163.com.

Interdisciplinary
-
Cross-referral requested
-
Research group
A - Aerospace Engineering
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-