Page 1 | Search Results | ASME Digital Collection

1-12 of 12

Sort by

Sort Order Select

Proceedings Papers

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

Proc. ASME. GT1993, Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery, V001T03A061, May 24–27, 1993

Publisher: American Society of Mechanical Engineers

Paper No: 93-GT-139

https://doi.org/10.1115/93-GT-139

View Paper titled, Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

Topics: Nozzles, Pressure, Shock waves, Shock (Mechanics), Pressure transducers, Excitation, Blades, Boundary layers, Flow (Dynamics), Flow visualization

Proceedings Papers

The Influence of Tailboards on Unsteady Measurements in a Linear Cascade

P. Ott, M. Norryd, A. Bölcs

Proc. ASME. GT1998, Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education, V005T14A050, June 2–5, 1998

Publisher: American Society of Mechanical Engineers

Paper No: 98-GT-572

https://doi.org/10.1115/98-GT-572

View Paper titled, The Influence of Tailboards on Unsteady Measurements in a Linear Cascade

Topics: Cascades (Fluid dynamics), Blades, Flow (Dynamics), Shock (Mechanics), Steady state, Test facilities, Transonic flow, Unsteady flow, Computation, Inviscid flow

Proceedings Papers

Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi 3D Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration

T. H. Fransson, M. Jöcker, A. Bölcs, P. Ott

Proc. ASME. GT1998, Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education, V005T14A043, June 2–5, 1998

Publisher: American Society of Mechanical Engineers

Paper No: 98-GT-490

https://doi.org/10.1115/98-GT-490

View Paper titled, Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi 3D Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration

Topics: Axial flow, Blades, Bubbles, Cascades (Fluid dynamics), Chords (Trusses), Computer simulation, Damping, Design, Engineering standards, Flow (Dynamics)

Proceedings Papers

Experimental and Numerical Study of the Thermal Performance of a Film Cooled Turbine Platform

D. Charbonnier, P. Ott, M. Jonsson, F. Cottier, Th. Ko¨bke

Proc. ASME. GT2009, Volume 3: Heat Transfer, Parts A and B, 1027-1038, June 8–12, 2009

Publisher: American Society of Mechanical Engineers

Paper No: GT2009-60306

https://doi.org/10.1115/GT2009-60306

View Paper titled, Experimental and Numerical Study of the Thermal Performance of a Film Cooled Turbine Platform

Topics: Turbines, Flow (Dynamics), Cooling, Coolants, Film cooling, Nozzle guide vanes, Engines, Pressure, Approximation, Carbon dioxide

Proceedings Papers

Comparison of Numerical Investigations With Measured Heat Transfer Performance of a Film Cooled Turbine Vane

D. Charbonnier, P. Ott, M. Jonsson, Th. Ko¨bke, F. Cottier

Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 571-582, June 9–13, 2008

Publisher: American Society of Mechanical Engineers

Paper No: GT2008-50623

https://doi.org/10.1115/GT2008-50623

View Paper titled, Comparison of Numerical Investigations With Measured Heat Transfer Performance of a Film Cooled Turbine Vane

Topics: Heat transfer, Turbines, Cooling, Film cooling, Flow (Dynamics), Nozzle guide vanes, Airfoils, Computation, Coolants, Heat transfer coefficients

Proceedings Papers

Application of the Transient Heater Foil Technique for Heat Transfer and Film Cooling Effectiveness Measurements on a Turbine Vane Endwall

M. Jonsson, D. Charbonnier, P. Ott, J. von Wolfersdorf

Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 443-453, June 9–13, 2008

Publisher: American Society of Mechanical Engineers

Paper No: GT2008-50451

https://doi.org/10.1115/GT2008-50451

View Paper titled, Application of the Transient Heater Foil Technique for Heat Transfer and Film Cooling Effectiveness Measurements on a Turbine Vane Endwall

Topics: Film cooling, Heat transfer, Transients (Dynamics), Turbines, Heat, Cascades (Fluid dynamics), Coolants, Flow (Dynamics), Temperature, Air flow

Proceedings Papers

Boundary Layer Suction via a Slot in a Transonic Compressor: Numerical Parameter Study and First Experiments

K. Hubrich, A. Bo¨lcs, P. Ott

Proc. ASME. GT2004, Volume 5: Turbo Expo 2004, Parts A and B, 527-536, June 14–17, 2004

Publisher: American Society of Mechanical Engineers

Paper No: GT2004-53758

https://doi.org/10.1115/GT2004-53758

View Paper titled, Boundary Layer Suction via a Slot in a Transonic Compressor: Numerical Parameter Study and First Experiments

Topics: Boundary layers, Compressors, Suction, Flow (Dynamics), Mach number, Pressure, Shock (Mechanics), Blades, Computation, Shock waves

Proceedings Papers

The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

G. Wagner, M. Kotulla, P. Ott, B. Weigand, J. von Wolfersdorf

Proc. ASME. GT2004, Volume 3: Turbo Expo 2004, 521-531, June 14–17, 2004

Publisher: American Society of Mechanical Engineers

Paper No: GT2004-53553

https://doi.org/10.1115/GT2004-53553

View Paper titled, The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

Topics: Liquid crystals, Transients (Dynamics), Wall thickness, Cylinders, Flat plates, Heat transfer, Blades, Gas turbines, Heat, Heat transfer coefficients

Journal Articles

Erratum: “The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness” [ Journal of Turbomachinery, 2005, 127(1), pp. 175–182 ]

G. Wagner, M. Kottula, P. Ott, B. Weigand, J. von Wolfersdorf

Publisher: ASME

J. Turbomach. October 2005, 127(4): 771–772.

https://doi.org/10.1115/1.2019348

Published Online: October 1, 2005

View Article titled, Erratum: “The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness” [ Journal of Turbomachinery, 2005, 127(1), pp. 175–182 ]

Topics: Liquid crystals, Transients (Dynamics), Turbomachinery, Wall thickness, Plates (structures)

Journal Articles

The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

G. Wagner, M. Kotulla, P. Ott, B. Weigand, J. von Wolfersdorf

Publisher: ASME

J. Turbomach. January 2005, 127(1): 175–182.

https://doi.org/10.1115/1.1811089

Published Online: February 9, 2005

View Article titled, The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

Topics: Cylinders, Flat plates, Heat transfer, Heat transfer coefficients, Liquid crystals, Temperature, Transients (Dynamics), Wall thickness, Gas turbines, Errors

Journal Articles

Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi-Three-Dimensional Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration

T. H. Fransson, M. Jo¨cker, A. Bo¨lcs, P. Ott

Publisher: ASME

J. Turbomach. October 1999, 121(4): 717–725.

https://doi.org/10.1115/1.2836725

Published Online: October 1, 1999

View Article titled, Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi-Three-Dimensional Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration

Topics: Axial flow, Blades, Bubbles, Cascades (Fluid dynamics), Chords (Trusses), Computer simulation, Damping, Design, Engineering standards, Flow (Dynamics)

Journal Articles

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

P. Ott, A. Bo¨lcs, T. H. Fransson

Publisher: ASME

J. Turbomach. January 1995, 117(1): 106–114.

https://doi.org/10.1115/1.2835625

Published Online: January 1, 1995

View Article titled, Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

Topics: Nozzles, Pressure, Shock waves, Shock (Mechanics), Pressure transducers, Excitation, Blades, Boundary layers, Flow (Dynamics), Flow visualization

Journal citation

NARROW

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

The Influence of Tailboards on Unsteady Measurements in a Linear Cascade

Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi 3D Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration

Experimental and Numerical Study of the Thermal Performance of a Film Cooled Turbine Platform

Comparison of Numerical Investigations With Measured Heat Transfer Performance of a Film Cooled Turbine Vane

Application of the Transient Heater Foil Technique for Heat Transfer and Film Cooling Effectiveness Measurements on a Turbine Vane Endwall

Boundary Layer Suction via a Slot in a Transonic Compressor: Numerical Parameter Study and First Experiments

The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

Erratum: “The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness” [ Journal of Turbomachinery, 2005, 127(1), pp. 175–182 ]

The Transient Liquid Crystal Technique: Influence of Surface Curvature and Finite Wall Thickness

Viscous and Inviscid Linear/Nonlinear Calculations Versus Quasi-Three-Dimensional Experimental Cascade Data for a New Aeroelastic Turbine Standard Configuration

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

ASME Journals

ASME Conference Proceedings

ASME eBooks

Resources

Opportunities

ASME Journals

ASME Conference Proceedings

ASME eBooks

Resources

Opportunities

This Feature Is Available To Subscribers Only