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Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response

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Published/Copyright: September 1, 1992
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International Journal of Turbo and Jet Engines
From the journal International Journal of Turbo and Jet Engines Volume 9 Issue 3

Published Online: 1992-09

©2011 by Walter de Gruyter GmbH & Co.

Articles in the same Issue

  1. CONTENTS
  2. Three-Dimensional Viscous Flow Through a Highly Loaded Compressor Rotor
  3. Studies on the Effect of Turbulence on the Spreading Rates of Bluff-Body Stabilized Flames
  4. Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response
  5. Semi-Analytical Fuel Injector Performance Correlation Approach
  6. Numerical Flow Analysis in Modern Gas Turbine Design
  7. Examination of Interactions Between Turbulence and Combustion in Diffusion Flame
  8. Three-Dimensional Incompressible Flow Solution of an Axial Compressor Using Pseudostream-Functions Formulation
https://doi.org/10.1515/TJJ.1992.9.3.191

Articles in the same Issue

  1. CONTENTS
  2. Three-Dimensional Viscous Flow Through a Highly Loaded Compressor Rotor
  3. Studies on the Effect of Turbulence on the Spreading Rates of Bluff-Body Stabilized Flames
  4. Nonuniform Upstream Airfoil Spacing Effects on Rotor Blade Noise Generation and Forced Response
  5. Semi-Analytical Fuel Injector Performance Correlation Approach
  6. Numerical Flow Analysis in Modern Gas Turbine Design
  7. Examination of Interactions Between Turbulence and Combustion in Diffusion Flame
  8. Three-Dimensional Incompressible Flow Solution of an Axial Compressor Using Pseudostream-Functions Formulation
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