Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor

Minsuk Choi,; JunYoung Park,; JeHyun Baek,

doi:10.1515/TJJ.2006.23.1.51

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Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor

Minsuk Choi, , JunYoung Park, und JeHyun Baek,

Veröffentlicht/Copyright: 1. März 2006

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Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 23 Heft 1

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Harvard
Chicago
Vancouver

Choi,, Minsuk, Park,, JunYoung and Baek,, JeHyun. "Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor" International Journal of Turbo and Jet Engines, vol. 23, no. 1, 2006, pp. 51-72. https://doi.org/10.1515/TJJ.2006.23.1.51

Choi,, M., Park,, J. & Baek,, J. (2006). Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor. International Journal of Turbo and Jet Engines, 23(1), 51-72. https://doi.org/10.1515/TJJ.2006.23.1.51

Choi,, M., Park,, J. and Baek,, J. (2006) Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor. International Journal of Turbo and Jet Engines, Vol. 23 (Issue 1), pp. 51-72. https://doi.org/10.1515/TJJ.2006.23.1.51

Choi,, Minsuk, Park,, JunYoung and Baek,, JeHyun. "Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor" International Journal of Turbo and Jet Engines 23, no. 1 (2006): 51-72. https://doi.org/10.1515/TJJ.2006.23.1.51

Choi, M, Park, J, Baek, J. Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor. International Journal of Turbo and Jet Engines. 2006;23(1): 51-72. https://doi.org/10.1515/TJJ.2006.23.1.51

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Published Online: 2006-03

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Artikel in diesem Heft

CONTENTS
Numerical Investigation of Unsteady Flow in a Low Pressure Turbine
A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers
Numerical Research on the Three Dimensional Unsteady Flow within the Vortex Pump
Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts
Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor

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https://doi.org/10.1515/TJJ.2006.23.1.51

Artikel in diesem Heft

CONTENTS
Numerical Investigation of Unsteady Flow in a Low Pressure Turbine
A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers
Numerical Research on the Three Dimensional Unsteady Flow within the Vortex Pump
Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts
Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor