Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine

Minsuk Choi,; Jong II Park,; Hee Taeg Chung,; Je Hun Baek,

doi:10.1515/TJJ.2009.26.2.97

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Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine

Minsuk Choi, , Jong II Park, , Hee Taeg Chung, and Je Hun Baek,

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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MLA
APA
Harvard
Chicago
Vancouver

Choi,, Minsuk, Park,, Jong II, Chung,, Hee Taeg and Baek,, Je Hun. "Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine" International Journal of Turbo and Jet Engines, vol. 26, no. 2, pp. 97-110. https://doi.org/10.1515/TJJ.2009.26.2.97

Choi,, M., Park,, J., Chung,, H. & Baek,, J. (). Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine. International Journal of Turbo and Jet Engines, 26(2), 97-110. https://doi.org/10.1515/TJJ.2009.26.2.97

Choi,, M., Park,, J., Chung,, H. and Baek,, J. () Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine. International Journal of Turbo and Jet Engines, Vol. 26 (Issue 2), pp. 97-110. https://doi.org/10.1515/TJJ.2009.26.2.97

Choi,, Minsuk, Park,, Jong II, Chung,, Hee Taeg and Baek,, Je Hun. "Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine" International Journal of Turbo and Jet Engines 26, no. 2 (): 97-110. https://doi.org/10.1515/TJJ.2009.26.2.97

Choi, M, Park, J, Chung, H, Baek, J. Relation of Clocking Effect and Secondary Flow in a 1.5 Stage Axial Turbine. International Journal of Turbo and Jet Engines. ;26(2): 97-110. https://doi.org/10.1515/TJJ.2009.26.2.97

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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

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https://doi.org/10.1515/TJJ.2009.26.2.97

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