A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow

Gao-Lien Liu,

doi:10.1515/TJJ.2004.21.1.29

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A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow

Gao-Lien Liu,

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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Harvard
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Vancouver

Liu,, Gao-Lien. "A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow" International Journal of Turbo and Jet Engines, vol. 21, no. 1, 2004, pp. 29-38. https://doi.org/10.1515/TJJ.2004.21.1.29

Liu,, G. (2004). A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow. International Journal of Turbo and Jet Engines, 21(1), 29-38. https://doi.org/10.1515/TJJ.2004.21.1.29

Liu,, G. (2004) A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow. International Journal of Turbo and Jet Engines, Vol. 21 (Issue 1), pp. 29-38. https://doi.org/10.1515/TJJ.2004.21.1.29

Liu,, Gao-Lien. "A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow" International Journal of Turbo and Jet Engines 21, no. 1 (2004): 29-38. https://doi.org/10.1515/TJJ.2004.21.1.29

Liu, G. A Coupled Aerothermoelastic Theory of Vibrating Blade-Fluid Interaction in Fully 3-D Transonic Rotor Flow. International Journal of Turbo and Jet Engines. 2004;21(1): 29-38. https://doi.org/10.1515/TJJ.2004.21.1.29

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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.2004.21.1.29

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