Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades

Brian H. Dennis,; IgorN. Yegorov-Egorov,; Helmut Sobieczky,; George S. Dulikravich,; Shinobu Yoshimura,

doi:10.1515/TJJ.2004.21.1.57

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Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades

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Published/Copyright: March 1, 2004

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From the journal International Journal of Turbo and Jet Engines Volume 21 Issue 1

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Dennis,, Brian H., Yegorov-Egorov,, IgorN., Sobieczky,, Helmut, Dulikravich,, George S. and Yoshimura,, Shinobu. "Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades" International Journal of Turbo and Jet Engines, vol. 21, no. 1, pp. 57-68. https://doi.org/10.1515/TJJ.2004.21.1.57

Dennis,, B., Yegorov-Egorov,, I., Sobieczky,, H., Dulikravich,, G. & Yoshimura,, S. (). Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades. International Journal of Turbo and Jet Engines, 21(1), 57-68. https://doi.org/10.1515/TJJ.2004.21.1.57

Dennis,, B., Yegorov-Egorov,, I., Sobieczky,, H., Dulikravich,, G. and Yoshimura,, S. () Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades. International Journal of Turbo and Jet Engines, Vol. 21 (Issue 1), pp. 57-68. https://doi.org/10.1515/TJJ.2004.21.1.57

Dennis,, Brian H., Yegorov-Egorov,, IgorN., Sobieczky,, Helmut, Dulikravich,, George S. and Yoshimura,, Shinobu. "Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades" International Journal of Turbo and Jet Engines 21, no. 1 (): 57-68. https://doi.org/10.1515/TJJ.2004.21.1.57

Dennis, B, Yegorov-Egorov, I, Sobieczky, H, Dulikravich, G, Yoshimura, S. Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages In Turbine Blades. International Journal of Turbo and Jet Engines. ;21(1): 57-68. https://doi.org/10.1515/TJJ.2004.21.1.57

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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

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https://doi.org/10.1515/TJJ.2004.21.1.57

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