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Proceedings Papers

Integrated Gas Turbine Technology Education at Durham University

Harry Marsh, Robert Dominy, David Gregory-Smith, Li He

Proc. ASME. GT1996, Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; General, V005T16A005, June 10–13, 1996

Paper No: 96-GT-192

DOI: https://doi.org/10.1115/96-GT-192

View Paper titled, Integrated Gas Turbine Technology Education at Durham University

Topics: Education, Gas turbines, Turbomachinery, Flow (Dynamics), Teaching, Turbines, Aerodynamics, Computers, Engineering education, Students

Proceedings Papers

Large Tip Clearance Flows in Two Compressor Cascades

Richard Williams, Grant Ingram, David Gregory-Smith

Proc. ASME. GT2010, Volume 7: Turbomachinery, Parts A, B, and C, 391-402, June 14–18, 2010

Paper No: GT2010-22952

DOI: https://doi.org/10.1115/GT2010-22952

View Paper titled, Large Tip Clearance Flows in Two Compressor Cascades

Topics: Clearances (Engineering), Compressors, Flow (Dynamics), Cascades (Fluid dynamics), Blades, Geometry, High pressure (Physics), Boundary layers, Design, Diffusion (Physics)

Proceedings Papers

The Performance of a Generic Non-Axisymmetric End Wall in a Single Stage, Rotating Turbine at On and Off-Design Conditions

Glen Snedden, Dwain Dunn, Grant Ingram, David Gregory-Smith

Proc. ASME. GT2010, Volume 7: Turbomachinery, Parts A, B, and C, 1069-1080, June 14–18, 2010

Paper No: GT2010-22006

DOI: https://doi.org/10.1115/GT2010-22006

View Paper titled, The Performance of a Generic Non-Axisymmetric End Wall in a Single Stage, Rotating Turbine at On and Off-Design Conditions

Topics: Design, Turbines, Computational fluid dynamics, Flow (Dynamics), Rotors, Energy generation, Engines, Probes, Stress

Proceedings Papers

The Application of Non-Axisymmetric Endwall Contouring in a Single Stage, Rotating Turbine

Glen Snedden, Dwain Dunn, Grant Ingram, David Gregory-Smith

Proc. ASME. GT2009, Volume 7: Turbomachinery, Parts A and B, 831-840, June 8–12, 2009

Paper No: GT2009-59169

DOI: https://doi.org/10.1115/GT2009-59169

View Paper titled, The Application of Non-Axisymmetric Endwall Contouring in a Single Stage, Rotating Turbine

Topics: Turbines, Flow (Dynamics), Computational fluid dynamics, Rotors, Clearances (Engineering), Design, Engines, Machinery, Pressure gradient, Probes

Journal Articles

Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade

Richard Williams, David Gregory-Smith, Li He, Grant Ingram

J. Turbomach. April 2010, 132(2): 021018.

DOI: https://doi.org/10.1115/1.3104611

Published Online: January 20, 2010

View Article titled, Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade

Topics: Blades, Cascades (Fluid dynamics), Clearances (Engineering), Flow (Dynamics), Pressure, Computational fluid dynamics, Vortices

Proceedings Papers

Using Profiled Endwalls, Blade Lean and Leading Edge Extensions to Minimize Secondary Flow

David Gregory-Smith, David Bagshaw, Grant Ingram, Mark Stokes

Proc. ASME. GT2008, Volume 6: Turbomachinery, Parts A, B, and C, 1301-1311, June 9–13, 2008

Paper No: GT2008-50811

DOI: https://doi.org/10.1115/GT2008-50811

View Paper titled, Using Profiled Endwalls, Blade Lean and Leading Edge Extensions to Minimize Secondary Flow

Topics: Blades, Flow (Dynamics), Pressure gradient, Engineering design processes, Turbines

Proceedings Papers

Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade

Richard Williams, David Gregory-Smith, Li He, Grant Ingram

Proc. ASME. GT2008, Volume 6: Turbomachinery, Parts A, B, and C, 335-347, June 9–13, 2008

Paper No: GT2008-50557

DOI: https://doi.org/10.1115/GT2008-50557

View Paper titled, Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade

Topics: Cascades (Fluid dynamics), Clearances (Engineering), Computation, Blades, Compressors, Flow (Dynamics), Design, Industrial gases, Pressure, Turbines

Proceedings Papers

A Design Method for the Profiling of End Walls in Turbines

Jonathan Hartland, David Gregory-Smith

Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 697-704, June 3–6, 2002

Paper No: GT2002-30433

DOI: https://doi.org/10.1115/GT2002-30433

View Paper titled, A Design Method for the Profiling of End Walls in Turbines

Topics: Design methodology, Turbines, Blades, Flow (Dynamics), Kinetic energy, Computational fluid dynamics, Cascades (Fluid dynamics), Design, Pressure gradient, Testing

Proceedings Papers

The Effect of End-Wall Profiling on Secondary Flow and Loss Development in a Turbine Cascade

Grant Ingram, David Gregory-Smith, Martin Rose, Neil Harvey, Graham Brennan

Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 135-145, June 3–6, 2002

Paper No: GT2002-30339

DOI: https://doi.org/10.1115/GT2002-30339

View Paper titled, The Effect of End-Wall Profiling on Secondary Flow and Loss Development in a Turbine Cascade

Topics: Cascades (Fluid dynamics), Flow (Dynamics), Turbines, Blades, Computational fluid dynamics, Design, Vortices

Proceedings Papers

Investigation of a Novel Secondary Flow Feature in a Turbine Cascade With End Wall Profiling

Grant Ingram, David Gregory-Smith, Neil Harvey

Proc. ASME. GT2004, Volume 5: Turbo Expo 2004, Parts A and B, 1199-1209, June 14–17, 2004

Paper No: GT2004-53589

DOI: https://doi.org/10.1115/GT2004-53589

View Paper titled, Investigation of a Novel Secondary Flow Feature in a Turbine Cascade With End Wall Profiling

Topics: Cascades (Fluid dynamics), Flow (Dynamics), Turbines, Computational fluid dynamics, Vortices, Blades, Boundary layers, Flow visualization, Kinetic energy, Pressure

Proceedings Papers

A Study of Large Tip Clearance Flows in an Axial Compressor Blade Row

Richard Williams, David Gregory-Smith, Li He

Proc. ASME. GT2006, Volume 6: Turbomachinery, Parts A and B, 251-259, May 8–11, 2006

Paper No: GT2006-90463

DOI: https://doi.org/10.1115/GT2006-90463

View Paper titled, A Study of Large Tip Clearance Flows in an Axial Compressor Blade Row

Topics: Blades, Clearances (Engineering), Compressors, Flow (Dynamics), Vortices, Cascades (Fluid dynamics), Pressure, Computational methods, Degrees of freedom, High pressure (Physics)

Journal Articles

Investigation of a Novel Secondary Flow Feature in a Turbine Cascade With End Wall Profiling

Grant Ingram, David Gregory-Smith, Neil Harvey

J. Turbomach. January 2005, 127(1): 209–214.

DOI: https://doi.org/10.1115/1.1812321

Published Online: February 9, 2005

View Article titled, Investigation of a Novel Secondary Flow Feature in a Turbine Cascade With End Wall Profiling

Topics: Cascades (Fluid dynamics), Computational fluid dynamics, Design, Flow (Dynamics), Turbines, Flow visualization, Blades, Boundary layers, Vortices

Journal citation

NARROW

Integrated Gas Turbine Technology Education at Durham University

Large Tip Clearance Flows in Two Compressor Cascades

The Performance of a Generic Non-Axisymmetric End Wall in a Single Stage, Rotating Turbine at On and Off-Design Conditions

The Application of Non-Axisymmetric Endwall Contouring in a Single Stage, Rotating Turbine

Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade

Using Profiled Endwalls, Blade Lean and Leading Edge Extensions to Minimize Secondary Flow

Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade

A Design Method for the Profiling of End Walls in Turbines

The Effect of End-Wall Profiling on Secondary Flow and Loss Development in a Turbine Cascade

Investigation of a Novel Secondary Flow Feature in a Turbine Cascade With End Wall Profiling

A Study of Large Tip Clearance Flows in an Axial Compressor Blade Row

Investigation of a Novel Secondary Flow Feature in a Turbine Cascade With End Wall Profiling

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