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Compressor Blade Row Unsteady Aerodynamic Response to Attached and Separated Flow Forcing Functions

  • K.H. Kim, and S. Fleeter,
Published/Copyright: September 1, 1994
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International Journal of Turbo and Jet Engines
From the journal International Journal of Turbo and Jet Engines Volume 11 Issue 2-3

Published Online: 1994-09

©2011 by Walter de Gruyter GmbH & Co.

Articles in the same Issue

  1. CONTENTS
  2. Editorial
  3. Thrust Vectoring For Flight Control & Safety: A Review
  4. Turbine Rotor Generated Forcing Functions for Flow Induced Vibrations
  5. The Mixing of Supersonic Jets in Subsonic Crossflow
  6. Forced Response Unsteady Aerodynamic Experiments
  7. Blade Arrangement Strategies for Minimal Rotor Unbalance
  8. Compressor Blade Row Unsteady Aerodynamic Response to Attached and Separated Flow Forcing Functions
  9. Performance Characteristics of Controllable Flat-Plate Flameholders
  10. Active Unsteady Aerodynamic Suppression of Rotating Stall in an Incompressible Flow Centrifugal Compressor with Vaned Diffuser
  11. Coating Growth on Turbine Blade in Polydisperse Particles/Hot Gas Flow
  12. Oscillating Flaps for Control of Turbomachine Wake Generated Discrete Frequency Noise
https://doi.org/10.1515/TJJ.1994.11.2-3.201

Articles in the same Issue

  1. CONTENTS
  2. Editorial
  3. Thrust Vectoring For Flight Control & Safety: A Review
  4. Turbine Rotor Generated Forcing Functions for Flow Induced Vibrations
  5. The Mixing of Supersonic Jets in Subsonic Crossflow
  6. Forced Response Unsteady Aerodynamic Experiments
  7. Blade Arrangement Strategies for Minimal Rotor Unbalance
  8. Compressor Blade Row Unsteady Aerodynamic Response to Attached and Separated Flow Forcing Functions
  9. Performance Characteristics of Controllable Flat-Plate Flameholders
  10. Active Unsteady Aerodynamic Suppression of Rotating Stall in an Incompressible Flow Centrifugal Compressor with Vaned Diffuser
  11. Coating Growth on Turbine Blade in Polydisperse Particles/Hot Gas Flow
  12. Oscillating Flaps for Control of Turbomachine Wake Generated Discrete Frequency Noise
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