An Integrated Approach to Gas Turbine Monitoring and Diagnostics

Igor Loboda,; Sergey Yepifanov,; Yakov Felshteyn,

doi:10.1515/TJJ.2009.26.2.111

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An Integrated Approach to Gas Turbine Monitoring and Diagnostics

Igor Loboda, , Sergey Yepifanov, and Yakov Felshteyn,

Published/Copyright: June 1, 2009

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From the journal International Journal of Turbo and Jet Engines Volume 26 Issue 2

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APA
Harvard
Chicago
Vancouver

Loboda,, Igor, Yepifanov,, Sergey and Felshteyn,, Yakov. "An Integrated Approach to Gas Turbine Monitoring and Diagnostics" International Journal of Turbo and Jet Engines, vol. 26, no. 2, pp. 111-126. https://doi.org/10.1515/TJJ.2009.26.2.111

Loboda,, I., Yepifanov,, S. & Felshteyn,, Y. (). An Integrated Approach to Gas Turbine Monitoring and Diagnostics. International Journal of Turbo and Jet Engines, 26(2), 111-126. https://doi.org/10.1515/TJJ.2009.26.2.111

Loboda,, I., Yepifanov,, S. and Felshteyn,, Y. () An Integrated Approach to Gas Turbine Monitoring and Diagnostics. International Journal of Turbo and Jet Engines, Vol. 26 (Issue 2), pp. 111-126. https://doi.org/10.1515/TJJ.2009.26.2.111

Loboda,, Igor, Yepifanov,, Sergey and Felshteyn,, Yakov. "An Integrated Approach to Gas Turbine Monitoring and Diagnostics" International Journal of Turbo and Jet Engines 26, no. 2 (): 111-126. https://doi.org/10.1515/TJJ.2009.26.2.111

Loboda, I, Yepifanov, S, Felshteyn, Y. An Integrated Approach to Gas Turbine Monitoring and Diagnostics. International Journal of Turbo and Jet Engines. ;26(2): 111-126. https://doi.org/10.1515/TJJ.2009.26.2.111

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CONTENTS
Experimental Study on a Two-phase Pulse Detonation Rocket Engine at the Frequency of 35Hz
Theoretical Calculation of Stability for NASA Stage 57 Rotor
Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine
An Integrated Approach to Gas Turbine Monitoring and Diagnostics
Microturbine Performance Testing using Biodiesel
Relationship between Shock-cell Length and Noise of Jets from Rectangular and Elliptic Disk Nozzles

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https://doi.org/10.1515/TJJ.2009.26.2.111

Articles in the same Issue

CONTENTS
Experimental Study on a Two-phase Pulse Detonation Rocket Engine at the Frequency of 35Hz
Theoretical Calculation of Stability for NASA Stage 57 Rotor
Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine
An Integrated Approach to Gas Turbine Monitoring and Diagnostics
Microturbine Performance Testing using Biodiesel
Relationship between Shock-cell Length and Noise of Jets from Rectangular and Elliptic Disk Nozzles