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The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade
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Vaclav Cyrus,
Published/Copyright:
June 1, 1992
Published Online: 1992-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade
- Direct Numerical Simulation of the Phase Change and Heat Transfer of a Vaporizing Droplet
- Loading Effects on the Aerodynamics of an Annular Cascade of Three Dimensional Airf
- Shock Wave/Free Shear Layer Interaction
- Effects of Pressure Mismatch on Slot Injection in Supersonic Flow
- A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers
- Calculation of the Flow Along the SI Stream Surface with Inviscid-Viscous Interaction Method
Articles in the same Issue
- CONTENTS
- The Effect of the Reynolds Number on the Three-Dimensional Flow in a Straight Compressor Cascade
- Direct Numerical Simulation of the Phase Change and Heat Transfer of a Vaporizing Droplet
- Loading Effects on the Aerodynamics of an Annular Cascade of Three Dimensional Airf
- Shock Wave/Free Shear Layer Interaction
- Effects of Pressure Mismatch on Slot Injection in Supersonic Flow
- A Method for Calculating Axial Turbomachine End Wall Turbulent Boundary Layers
- Calculation of the Flow Along the SI Stream Surface with Inviscid-Viscous Interaction Method
