Microturbine Performance Testing with Twin Rotating Disk Regenerators

H.-W.D. Chiang,; W.-T. Hong,; C.-H. Lee,

doi:10.1515/TJJ.2007.24.3-4.137

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Microturbine Performance Testing with Twin Rotating Disk Regenerators

H.-W.D. Chiang, , W.-T. Hong, und C.-H. Lee,

Veröffentlicht/Copyright: 1. Dezember 2007

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 24 Heft 3-4

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Harvard
Chicago
Vancouver

Chiang,, H.-W.D., Hong,, W.-T. and Lee,, C.-H.. "Microturbine Performance Testing with Twin Rotating Disk Regenerators" International Journal of Turbo and Jet Engines, vol. 24, no. 3-4, pp. 137-160. https://doi.org/10.1515/TJJ.2007.24.3-4.137

Chiang,, H., Hong,, W. & Lee,, C. (). Microturbine Performance Testing with Twin Rotating Disk Regenerators. International Journal of Turbo and Jet Engines, 24(3-4), 137-160. https://doi.org/10.1515/TJJ.2007.24.3-4.137

Chiang,, H., Hong,, W. and Lee,, C. () Microturbine Performance Testing with Twin Rotating Disk Regenerators. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 3-4), pp. 137-160. https://doi.org/10.1515/TJJ.2007.24.3-4.137

Chiang,, H.-W.D., Hong,, W.-T. and Lee,, C.-H.. "Microturbine Performance Testing with Twin Rotating Disk Regenerators" International Journal of Turbo and Jet Engines 24, no. 3-4 (): 137-160. https://doi.org/10.1515/TJJ.2007.24.3-4.137

Chiang, H, Hong, W, Lee, C. Microturbine Performance Testing with Twin Rotating Disk Regenerators. International Journal of Turbo and Jet Engines. ;24(3-4): 137-160. https://doi.org/10.1515/TJJ.2007.24.3-4.137

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Published Online: 2007-12

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Artikel in diesem Heft

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.2007.24.3-4.137

Artikel in diesem Heft

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