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An Integrated Approach to Gas Turbine Monitoring and Diagnostics

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Veröffentlicht/Copyright: 1. Juni 2009
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International Journal of Turbo and Jet Engines
Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 26 Heft 2

Published Online: 2009-06

©2011 by Walter de Gruyter GmbH & Co.

Artikel in diesem Heft

  1. CONTENTS
  2. Experimental Study on a Two-phase Pulse Detonation Rocket Engine at the Frequency of 35Hz
  3. Theoretical Calculation of Stability for NASA Stage 57 Rotor
  4. Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine
  5. An Integrated Approach to Gas Turbine Monitoring and Diagnostics
  6. Microturbine Performance Testing using Biodiesel
  7. Relationship between Shock-cell Length and Noise of Jets from Rectangular and Elliptic Disk Nozzles
https://doi.org/10.1515/TJJ.2009.26.2.111

Artikel in diesem Heft

  1. CONTENTS
  2. Experimental Study on a Two-phase Pulse Detonation Rocket Engine at the Frequency of 35Hz
  3. Theoretical Calculation of Stability for NASA Stage 57 Rotor
  4. Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine
  5. An Integrated Approach to Gas Turbine Monitoring and Diagnostics
  6. Microturbine Performance Testing using Biodiesel
  7. Relationship between Shock-cell Length and Noise of Jets from Rectangular and Elliptic Disk Nozzles
Heruntergeladen am 1.5.2026 von https://www.degruyterbrill.com/document/doi/10.1515/TJJ.2009.26.2.111/html?lang=de
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