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, and JeHyun Baek,

Published/Copyright: March 1, 2006

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From the journal International Journal of Turbo and Jet Engines Volume 23 Issue 1

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Harvard
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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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Articles in the same Issue

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

Articles in the same Issue

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