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Experimental Evaluation of Precursors to Centrifugal Compressor Instability
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Patrick B. Lawless,
Published/Copyright:
December 1, 2000
Published Online: 2000-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows
- Characteristics of Arrays of Spray Diffusion Flames
- Maximizing Multistage Turbine Efficiency by Optimizing Hub and Shroud Shapes and Inlet and Exit Conditions of Each Blade Row
- Experimental Evaluation of Precursors to Centrifugal Compressor Instability
- 3-D Inlet Guide Vane Generated Vortical Forcing Functions
- Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance
- A New Era of Jet Transport Safety By Advanced Legislation?
Articles in the same Issue
- CONTENTS
- Experimental and Numerical Investigation of Losses in Low-Pressure Turbine Blade Rows
- Characteristics of Arrays of Spray Diffusion Flames
- Maximizing Multistage Turbine Efficiency by Optimizing Hub and Shroud Shapes and Inlet and Exit Conditions of Each Blade Row
- Experimental Evaluation of Precursors to Centrifugal Compressor Instability
- 3-D Inlet Guide Vane Generated Vortical Forcing Functions
- Effect of Space-Chord Ratio on the Endwall Flow in a Large Deflection Turbine Rotor Cascade with Tip Clearance
- A New Era of Jet Transport Safety By Advanced Legislation?
