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A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations

  • Wu Zhe-min, , Li Hong, und Liu Gao-lian,
Veröffentlicht/Copyright: 1. März 2004
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International Journal of Turbo and Jet Engines
Aus der Zeitschrift International Journal of Turbo and Jet Engines Band 21 Heft 1

Published Online: 2004-03

©2011 by Walter de Gruyter GmbH & Co.

Artikel in diesem Heft

  1. CONTENTS
  2. Passive Control of Underexpanded Jets
  3. Statistical Model of Casting Treatment Influence on Compressor Efficiency
  4. Laminar Forced Convection in Curved Channel with Vortex Structures
  5. A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow
  6. A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations
  7. Influence of Degradation and Inlet Distortion on Gas Turbine Performance
  8. Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades
https://doi.org/10.1515/TJJ.2004.21.1.39

Artikel in diesem Heft

  1. CONTENTS
  2. Passive Control of Underexpanded Jets
  3. Statistical Model of Casting Treatment Influence on Compressor Efficiency
  4. Laminar Forced Convection in Curved Channel with Vortex Structures
  5. A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow
  6. A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations
  7. Influence of Degradation and Inlet Distortion on Gas Turbine Performance
  8. Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades
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