Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model

C. Kong,; J. Ki,; S. Kho,; C. Lee,

doi:10.1515/TJJ.2007.24.3-4.161

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Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model

C. Kong, , J. Ki, , S. Kho, and C. Lee,

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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Harvard
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Kong,, C., Ki,, J., Kho,, S. and Lee,, C.. "Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model" International Journal of Turbo and Jet Engines, vol. 24, no. 3-4, pp. 161-170. https://doi.org/10.1515/TJJ.2007.24.3-4.161

Kong,, C., Ki,, J., Kho,, S. & Lee,, C. (). Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model. International Journal of Turbo and Jet Engines, 24(3-4), 161-170. https://doi.org/10.1515/TJJ.2007.24.3-4.161

Kong,, C., Ki,, J., Kho,, S. and Lee,, C. () Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 3-4), pp. 161-170. https://doi.org/10.1515/TJJ.2007.24.3-4.161

Kong,, C., Ki,, J., Kho,, S. and Lee,, C.. "Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model" International Journal of Turbo and Jet Engines 24, no. 3-4 (): 161-170. https://doi.org/10.1515/TJJ.2007.24.3-4.161

Kong, C, Ki, J, Kho, S, Lee, C. Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model. International Journal of Turbo and Jet Engines. ;24(3-4): 161-170. https://doi.org/10.1515/TJJ.2007.24.3-4.161

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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.2007.24.3-4.161

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