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Active Unsteady Aerodynamic Suppression of Rotating Stall in an Incompressible Flow Centrifugal Compressor with Vaned Diffuser
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P.B. Lawless,
and S. Fleeter,
Published/Copyright:
September 1, 1994
Published Online: 1994-09
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Editorial
- Thrust Vectoring For Flight Control & Safety: A Review
- Turbine Rotor Generated Forcing Functions for Flow Induced Vibrations
- The Mixing of Supersonic Jets in Subsonic Crossflow
- Forced Response Unsteady Aerodynamic Experiments
- Blade Arrangement Strategies for Minimal Rotor Unbalance
- Compressor Blade Row Unsteady Aerodynamic Response to Attached and Separated Flow Forcing Functions
- Performance Characteristics of Controllable Flat-Plate Flameholders
- Active Unsteady Aerodynamic Suppression of Rotating Stall in an Incompressible Flow Centrifugal Compressor with Vaned Diffuser
- Coating Growth on Turbine Blade in Polydisperse Particles/Hot Gas Flow
- Oscillating Flaps for Control of Turbomachine Wake Generated Discrete Frequency Noise
Articles in the same Issue
- CONTENTS
- Editorial
- Thrust Vectoring For Flight Control & Safety: A Review
- Turbine Rotor Generated Forcing Functions for Flow Induced Vibrations
- The Mixing of Supersonic Jets in Subsonic Crossflow
- Forced Response Unsteady Aerodynamic Experiments
- Blade Arrangement Strategies for Minimal Rotor Unbalance
- Compressor Blade Row Unsteady Aerodynamic Response to Attached and Separated Flow Forcing Functions
- Performance Characteristics of Controllable Flat-Plate Flameholders
- Active Unsteady Aerodynamic Suppression of Rotating Stall in an Incompressible Flow Centrifugal Compressor with Vaned Diffuser
- Coating Growth on Turbine Blade in Polydisperse Particles/Hot Gas Flow
- Oscillating Flaps for Control of Turbomachine Wake Generated Discrete Frequency Noise