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Comparison of Counter-rotating and Traditional Axial Aircraft
Low-pressure Turbines Integral and Detailed Performances
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Int. Symp. on Heat Transfer in Gas Turbine Systems
9-14 August 2009, Antalya, Turkey
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Designing the Flowpath.
Robust and Efficient Aerodynamics and Structural Solvers Can Provide an Integrated Software Solution for Performing the Entire Workflow
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TURBOMACHINERY INTERNATIONAL,
The Global Journal of Energy Equipment,
March/April 2009, Vol.50 NO.2
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Integrated Conceptual Design Environment for Centrifugal Compressors Flow Path Design (2008)
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Proceedings of IMECE2008, 2008 ASME International Mechanical Engineering Congress and Exposition,
November 2-6, 2008, Boston, Massachusetts, USA
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Advanced Gas Turbine Concept, Design and Evaluation Methodology.
Preliminary Design of Highly Loaded
Low Pressure Gas Turbine of Engine (2007)
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Proceedings of the International Gas Turbine Congress 2007
Tokyo December 3-7, 2007
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A uniform approach to conceptual design of axial turbine / compressor flow path (2006)
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The Future of Gas Turbine Technology
3rd International Conference
11-12 October 2006, Brussels, Belgium
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Axial turbine stages design:
1D/2D/3D simulation, experiment, optimization
design of single stage test
air turbine models and
validation of 1D/2D/3D aerodynamic
computation results against test data. (2005)
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Proceedings of GT2005
ASME Turbo Expo 2005: Power for Land, Sea and Air
June 6-9, 2005, Reno-Tahoe, Nevada, USA
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Methods and tools for multidisciplinary optimization of axial turbine stages with relatively long blades (2004)
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Proceedings of ASME Turbo Expo 2004
Power for Land, Sea, and Air
June 14-17, 2004, Vienna, Austria
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Flow phenomenon in steam turbine disk-stator cavities channeled by balance holes (2004)
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Proceedings of ASME Turbo Expo 2004
Power for Land, Sea, and Air
June 14-17, 2004, Vienna, Austria
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Coupled CFD and thermal steady state analysis of steam turbine secondary flow path. (2003)
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IJPGC 2003 2003 International Joint Power Generation Conference
June 16-19, 2003, Atlanta, Georgia, USA
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