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Study Of Low Reynolds Number Effects On The Losses In Low-Pressure Turbine Blade Rows
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Daniel J. Dorney,
Veröffentlicht/Copyright:
1. Juni 1999
Published Online: 1999-06
©2011 by Walter de Gruyter GmbH & Co.
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Artikel in diesem Heft
- CONTENTS
- Technical Notes: Modern Experimental Techniques in Turbine Engine Testing
- Investigation of Separated Flow Around a Curved Air Intake
- The Effects Of Thermal Gradients On The Performance of Axial Compressors
- Study Of Low Reynolds Number Effects On The Losses In Low-Pressure Turbine Blade Rows
- Vortex Shedding in a Turbine Cascade
Artikel in diesem Heft
- CONTENTS
- Technical Notes: Modern Experimental Techniques in Turbine Engine Testing
- Investigation of Separated Flow Around a Curved Air Intake
- The Effects Of Thermal Gradients On The Performance of Axial Compressors
- Study Of Low Reynolds Number Effects On The Losses In Low-Pressure Turbine Blade Rows
- Vortex Shedding in a Turbine Cascade
