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Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades
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Brian H. Dennis,
Published/Copyright:
March 1, 2004
Published Online: 2004-03
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Passive Control of Underexpanded Jets
- Statistical Model of Casting Treatment Influence on Compressor Efficiency
- Laminar Forced Convection in Curved Channel with Vortex Structures
- A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow
- A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations
- Influence of Degradation and Inlet Distortion on Gas Turbine Performance
- Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades
Articles in the same Issue
- CONTENTS
- Passive Control of Underexpanded Jets
- Statistical Model of Casting Treatment Influence on Compressor Efficiency
- Laminar Forced Convection in Curved Channel with Vortex Structures
- A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow
- A New Characteristics-Based Finite Difference Method for Hyperbolic Partial Differential Equations
- Influence of Degradation and Inlet Distortion on Gas Turbine Performance
- Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades