Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor

O.G. Krishnakumar,; M. Govardhan,; N. Sitaram,

doi:10.1515/TJJ.2007.24.3-4.195

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Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor

O.G. Krishnakumar, , M. Govardhan, und N. Sitaram,

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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MLA
APA
Harvard
Chicago
Vancouver

Krishnakumar,, O.G., Govardhan,, M. and Sitaram,, N.. "Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor" International Journal of Turbo and Jet Engines, vol. 24, no. 3-4, pp. 195-206. https://doi.org/10.1515/TJJ.2007.24.3-4.195

Krishnakumar,, O., Govardhan,, M. & Sitaram,, N. (). Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor. International Journal of Turbo and Jet Engines, 24(3-4), 195-206. https://doi.org/10.1515/TJJ.2007.24.3-4.195

Krishnakumar,, O., Govardhan,, M. and Sitaram,, N. () Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor. International Journal of Turbo and Jet Engines, Vol. 24 (Issue 3-4), pp. 195-206. https://doi.org/10.1515/TJJ.2007.24.3-4.195

Krishnakumar,, O.G., Govardhan,, M. and Sitaram,, N.. "Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor" International Journal of Turbo and Jet Engines 24, no. 3-4 (): 195-206. https://doi.org/10.1515/TJJ.2007.24.3-4.195

Krishnakumar, O, Govardhan, M, Sitaram, N. Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor. International Journal of Turbo and Jet Engines. ;24(3-4): 195-206. https://doi.org/10.1515/TJJ.2007.24.3-4.195

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Published Online: 2007-12

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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.2007.24.3-4.195

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