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Journal Articles

A Remotely Operated Aeroelastically Unstable Low Pressure Turbine Cascade for Turbomachinery Aeromechanics Education and Training—Remote Flutter Lab

Monaco Lucio, John Bergmans, Damian Vogt, Torsten H. Fransson

Publisher: ASME

J. Eng. Gas Turbines Power. March 2015, 137(3): 032507.

Paper No: GTP-14-1382

https://doi.org/10.1115/1.4028463

Published Online: October 7, 2014

View Article titled, A Remotely Operated Aeroelastically Unstable Low Pressure Turbine Cascade for Turbomachinery Aeromechanics Education and Training—Remote Flutter Lab

Topics: Blades, Cascades (Fluid dynamics), Education, Flow (Dynamics), Flutter (Aerodynamics), Graphical user interfaces, Pressure, Students, Turbomachinery, Turbines

Journal Articles

Steady-State and Transient Performance Modeling of Smart UAV Propulsion System Using SIMULINK

Jayoung Ki, Changduk Kong, Seonghee Kho, Changho Lee

Publisher: ASME

J. Eng. Gas Turbines Power. May 2009, 131(3): 031702.

https://doi.org/10.1115/1.2982141

Published Online: February 10, 2009

View Article titled, Steady-State and Transient Performance Modeling of Smart UAV Propulsion System Using SIMULINK

Topics: Compressors, Engines, Generators, Modeling, Steady state, Transients (Dynamics), Turbines, Unmanned aerial vehicles, Temperature, Propulsion systems

Journal Articles

Preliminary Gas Turbine Design Using the Multidisciplinary Design System MOPEDS

P. Jeschke, J. Kurzke, R. Schaber, C. Riegler

Publisher: ASME

J. Eng. Gas Turbines Power. April 2004, 126(2): 258–264.

https://doi.org/10.1115/1.1639009

Published Online: June 7, 2004

View Article titled, Preliminary Gas Turbine Design Using the Multidisciplinary Design System MOPEDS

Topics: Design, Engines, Gas turbines, Graphical user interfaces

Journal Articles

Gas Turbine Cycle Design Methodology: A Comparison of Parameter Variation With Numerical Optimization

J. Kurzke

Publisher: ASME

J. Eng. Gas Turbines Power. January 1999, 121(1): 6–11.

https://doi.org/10.1115/1.2816315

Published Online: January 1, 1999

View Article titled, Gas Turbine Cycle Design Methodology: A Comparison of Parameter Variation With Numerical Optimization

Topics: Cycles, Design methodology, Gas turbines, Optimization, Design, Simulation, Engines, Graphical user interfaces, Optimization algorithms, Thermodynamic cycles

Journal citation

NARROW

A Remotely Operated Aeroelastically Unstable Low Pressure Turbine Cascade for Turbomachinery Aeromechanics Education and Training—Remote Flutter Lab

Steady-State and Transient Performance Modeling of Smart UAV Propulsion System Using SIMULINK

Preliminary Gas Turbine Design Using the Multidisciplinary Design System MOPEDS

Gas Turbine Cycle Design Methodology: A Comparison of Parameter Variation With Numerical Optimization

ASME Journals

ASME Conference Proceedings

ASME eBooks

Resources

Opportunities

A Remotely Operated Aeroelastically Unstable Low Pressure Turbine Cascade for Turbomachinery Aeromechanics Education and Training—Remote Flutter Lab

Steady-State and Transient Performance Modeling of Smart UAV Propulsion System Using SIMULINK

Preliminary Gas Turbine Design Using the Multidisciplinary Design System MOPEDS

Gas Turbine Cycle Design Methodology: A Comparison of Parameter Variation With Numerical Optimization

ASME Journals

ASME Conference Proceedings

ASME eBooks

Resources

Opportunities

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