Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method

C. Kong,; J. Ki,

doi:10.1515/TJJ.2007.24.3-4.171

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Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method

C. Kong, and J. Ki,

Published/Copyright: December 1, 2007

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From the journal International Journal of Turbo and Jet Engines Volume 24 Issue 3-4

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APA
Harvard
Chicago
Vancouver

Kong,, C. and Ki,, J.. "Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method" International Journal of Turbo and Jet Engines, vol. 24, no. 3-4, pp. 171-182. https://doi.org/10.1515/TJJ.2007.24.3-4.171

Kong,, C. & Ki,, J. (). Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method. International Journal of Turbo and Jet Engines, 24(3-4), 171-182. https://doi.org/10.1515/TJJ.2007.24.3-4.171

Kong,, C. and Ki,, J. () Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 3-4), pp. 171-182. https://doi.org/10.1515/TJJ.2007.24.3-4.171

Kong,, C. and Ki,, J.. "Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method" International Journal of Turbo and Jet Engines 24, no. 3-4 (): 171-182. https://doi.org/10.1515/TJJ.2007.24.3-4.171

Kong, C, Ki, J. Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method. International Journal of Turbo and Jet Engines. ;24(3-4): 171-182. https://doi.org/10.1515/TJJ.2007.24.3-4.171

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Published Online: 2007-12

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Articles in the same Issue

CONTENTS
Microturbine Performance Testing with Twin Rotating Disk Regenerators
Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model
Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method
A Phenomenological Two-Phase Flow Model of Atomization in an Internally Mixed Liquid Atomizer
Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor
An Experimental Investigation on the Airflow in Twin Submerged Side Intake at Subsonic Speeds
Low Frequencies and Growth of Oscillations in a Rijke Tube
Gas Turbine Diagnostics Under Variable Operating Conditions
Effect of the Second Stage on a Partially Admitted Small Turbine
Probabilistic Analysis of a Turbine Blade

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https://doi.org/10.1515/TJJ.2007.24.3-4.171

Articles in the same Issue

CONTENTS
Microturbine Performance Testing with Twin Rotating Disk Regenerators
Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model
Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method
A Phenomenological Two-Phase Flow Model of Atomization in an Internally Mixed Liquid Atomizer
Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor
An Experimental Investigation on the Airflow in Twin Submerged Side Intake at Subsonic Speeds
Low Frequencies and Growth of Oscillations in a Rijke Tube
Gas Turbine Diagnostics Under Variable Operating Conditions
Effect of the Second Stage on a Partially Admitted Small Turbine
Probabilistic Analysis of a Turbine Blade