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Aeroelastic Detuning for Stability Enhancement of Unstalled Supersonic Flutter

  • S. Fleeter, and D. Hoyniak,
Published/Copyright: March 1, 1989
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International Journal of Turbo and Jet Engines
From the journal International Journal of Turbo and Jet Engines Volume 6 Issue 1

Published Online: 1989-03

©2011 by Walter de Gruyter GmbH & Co.

Articles in the same Issue

  1. CONTENTS
  2. The Fundamentals of Vectored Propulsion
  3. Aeroelastic Detuning for Stability Enhancement of Unstalled Supersonic Flutter
  4. Stability of Conical and Curved Annular Diffusers for Mixed-Flow Compressors
  5. Design Objectives and Experience with Processor Based Gas Turbine Controls
  6. Local Measurement of Particle Concentration, Size and Velocity in the Sheet of a Flat Spray Nozzle with Double Pulse Holography
  7. Large Heavy-Duty Gas Turbines for Base-Load Power Generation and Heat Cogeneration
  8. A Finite Element Scheme for Incompressible Viscous Flow Calculations
  9. Numerical Study of a Dump Diffuser Flow Field in a Short Annular Combustor
  10. Experimental Investigation of Dynamic Distortion Properties in Transonic Flow Diffuser
  11. Computation of the Trailing Edge Flow Downstream A Flat Plate with Finite Thickness
https://doi.org/10.1515/TJJ.1989.6.1.17

Articles in the same Issue

  1. CONTENTS
  2. The Fundamentals of Vectored Propulsion
  3. Aeroelastic Detuning for Stability Enhancement of Unstalled Supersonic Flutter
  4. Stability of Conical and Curved Annular Diffusers for Mixed-Flow Compressors
  5. Design Objectives and Experience with Processor Based Gas Turbine Controls
  6. Local Measurement of Particle Concentration, Size and Velocity in the Sheet of a Flat Spray Nozzle with Double Pulse Holography
  7. Large Heavy-Duty Gas Turbines for Base-Load Power Generation and Heat Cogeneration
  8. A Finite Element Scheme for Incompressible Viscous Flow Calculations
  9. Numerical Study of a Dump Diffuser Flow Field in a Short Annular Combustor
  10. Experimental Investigation of Dynamic Distortion Properties in Transonic Flow Diffuser
  11. Computation of the Trailing Edge Flow Downstream A Flat Plate with Finite Thickness
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