Gas Turbine Diagnostics Under Variable Operating Conditions

I. Loboda,; Y. Feldshteyn,; S. Yepifanov,

doi:10.1515/TJJ.2007.24.3-4.231

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Gas Turbine Diagnostics Under Variable Operating Conditions

I. Loboda, , Y. Feldshteyn, and S. Yepifanov,

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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Vancouver

Loboda,, I., Feldshteyn,, Y. and Yepifanov,, S.. "Gas Turbine Diagnostics Under Variable Operating Conditions" International Journal of Turbo and Jet Engines, vol. 24, no. 3-4, pp. 231-244. https://doi.org/10.1515/TJJ.2007.24.3-4.231

Loboda,, I., Feldshteyn,, Y. & Yepifanov,, S. (). Gas Turbine Diagnostics Under Variable Operating Conditions. International Journal of Turbo and Jet Engines, 24(3-4), 231-244. https://doi.org/10.1515/TJJ.2007.24.3-4.231

Loboda,, I., Feldshteyn,, Y. and Yepifanov,, S. () Gas Turbine Diagnostics Under Variable Operating Conditions. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 3-4), pp. 231-244. https://doi.org/10.1515/TJJ.2007.24.3-4.231

Loboda,, I., Feldshteyn,, Y. and Yepifanov,, S.. "Gas Turbine Diagnostics Under Variable Operating Conditions" International Journal of Turbo and Jet Engines 24, no. 3-4 (): 231-244. https://doi.org/10.1515/TJJ.2007.24.3-4.231

Loboda, I, Feldshteyn, Y, Yepifanov, S. Gas Turbine Diagnostics Under Variable Operating Conditions. International Journal of Turbo and Jet Engines. ;24(3-4): 231-244. https://doi.org/10.1515/TJJ.2007.24.3-4.231

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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.2007.24.3-4.231

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