Nonlinear multiple points gas turbine off-design performance adaptation using a genetic algorithm

Journal of Engineering for Gas Turbines and Power

Volumn 133, Issue 7, 2011, Pages

  Li, Y G ^a   Ghafir, M F Abdul ^a   Wang, L ^a   Singh, R ^a   Huang, K ^b   Feng, X ^b  

^a CRANFIELD UNIVERSITY   (United Kingdom)

^b AVIATION INDUSTRY CORPORATION OF CHINA   (China)

Author keywords

[No Author keywords available]

Indexed keywords

AERO GAS TURBINE ENGINES; COMPONENT CHARACTERISTICS; DIAGNOSTIC APPLICATIONS; ENGINE COMPONENTS; ENGINE PERFORMANCE MODELS; GAS PATH; GAS TURBINE ENGINE; GAS TURBINE PERFORMANCE; GAS-PATH MEASUREMENTS; MULTIPLE POINTS; NON-LINEAR SCALING; NONLINEAR MAP; OBJECTIVE FUNCTIONS; OFF DESIGN CONDITION; OFF-DESIGN OPERATING CONDITIONS; OFF-DESIGN PERFORMANCE; OPTIMAL SETS; PERFORMANCE ADAPTATION; PERFORMANCE MODEL; PERFORMANCE PREDICTION; RIG TESTS; SCALING FACTORS; TEST DATA; THERMODYNAMIC PERFORMANCE;

CASCADES (FLUID MECHANICS); ENGINES; GASES; GENETIC ALGORITHMS; MACHINE DESIGN; TURBOMACHINERY;

GAS TURBINES;

EID: 79952751826     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.4002620     Document Type: Article

References (12)

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