Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method

A. Tourlidakis,; R.L. Elder,

doi:10.1515/TJJ.1996.13.1.35

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Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method

A. Tourlidakis, and R.L. Elder,

Published/Copyright: March 1, 1996

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From the journal International Journal of Turbo and Jet Engines Volume 13 Issue 1

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MLA
APA
Harvard
Chicago
Vancouver

Tourlidakis,, A. and Elder,, R.L.. "Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method" International Journal of Turbo and Jet Engines, vol. 13, no. 1, pp. 35-54. https://doi.org/10.1515/TJJ.1996.13.1.35

Tourlidakis,, A. & Elder,, R. (). Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method. International Journal of Turbo and Jet Engines, 13(1), 35-54. https://doi.org/10.1515/TJJ.1996.13.1.35

Tourlidakis,, A. and Elder,, R. () Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method. International Journal of Turbo and Jet Engines, Vol. 13 (Issue 1), pp. 35-54. https://doi.org/10.1515/TJJ.1996.13.1.35

Tourlidakis,, A. and Elder,, R.L.. "Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method" International Journal of Turbo and Jet Engines 13, no. 1 (): 35-54. https://doi.org/10.1515/TJJ.1996.13.1.35

Tourlidakis, A, Elder, R. Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method. International Journal of Turbo and Jet Engines. ;13(1): 35-54. https://doi.org/10.1515/TJJ.1996.13.1.35

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Published Online: 1996-03

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CONTENTS
Generalized Euler's Turbomachine Equation and Free Vortex Sheet Conditions in Separated/Cavitated Turbo-Flows
Variable-Domain Finite Element Method Based on Variational Principles for Solving Hybrid Problems of Fully 3-D Compressible Rotor-Flow
Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor
Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method
Active Control of Surge in Multi-Stage Axial-Flow Compressors
Technical Note: Performance of a Miniature Gas Turbine Engine

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https://doi.org/10.1515/TJJ.1996.13.1.35

Articles in the same Issue

CONTENTS
Generalized Euler's Turbomachine Equation and Free Vortex Sheet Conditions in Separated/Cavitated Turbo-Flows
Variable-Domain Finite Element Method Based on Variational Principles for Solving Hybrid Problems of Fully 3-D Compressible Rotor-Flow
Measurement of the Unsteady Flow at the Entrance to an Axial Gas Turbine Rotor
Numerical Investigations of Centrifugal Compressor Flows with Tip Leakage Using a Pressure Correction Method
Active Control of Surge in Multi-Stage Axial-Flow Compressors
Technical Note: Performance of a Miniature Gas Turbine Engine