Publications

Showing 22 out of 82 publications matching your search

Influence of Film Cooling Hole Angles and Geometries on Aerodynamic Loss and Net Heat Flux Reduction

Authors:

Chia Hui Lim; Graham Pullan; Peter Ireland

Publication:

J. Turbomach. 2013; 135(5):051019-051019-13.

DOI:

10.1115/1.4023088

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Stall Warning by Blade Pressure Signature Analysis

Authors:

Anna Young; Ivor Day; Graham Pullan

Publication:

J. Turbomach. 2012; 135(1):011033-011033-10.

DOI:

10.1115/1.4006426

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Estimating the Loss Associated With Film Cooling for a Turbine Stage

Authors:

Chia Hui Lim; Graham Pullan; John Northall

Publication:

J. Turbomach. 2011; 134(2):021011-021011-10.

DOI:

10.1115/1.4003255

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An Accelerated 3D Navier–Stokes Solver for Flows in Turbomachines

Authors:

Tobias Brandvik; Graham Pullan

Publication:

J. Turbomach. 2010; 133(2):021025-021025-9.

DOI:

doi: 10.1115/1.4001192

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SBLOCK: A Framework for Efficient Stencil-Based PDE Solvers on Multi-core Platforms

Authors:

Tobias Brandvik; Graham Pullan

Publication:

Proc. IEEE CIT 2010

DOI:

10.1109/CIT.2010.214

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The Influence of Sweep on Axial Flow Turbine Aerodynamics in the Endwall Region

Authors:

Graham Pullan; Neil W. Harvey

Publication:

J. Turbomach. 2008; 130(4):041011-041011-10.

DOI:

10.1115/1.2812337

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Acceleration of a 3D Euler Solver Using Commodity Graphics Hardware

Authors:

Tobias Brandvik; Graham Pullan

Publication:

AIAA 2008-607

DOI:

10.2514/6.2008-607

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The Interaction of Turbine Inter-Platform Leakage Flow With the Mainstream Flow

Authors:

Kevin Reid; John Denton; Graham Pullan; Eric Curtis; John Longley

Publication:

J. Turbomach. 2005; 129(2):303-310.

DOI:

10.1115/1.2162592

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The Importance of Shroud Leakage Modeling in Multistage Turbine Flow Calculations

Authors:

Budimir Rosic; John D. Denton; Graham Pullan

Publication:

J. Turbomach. 2005; 128(4):699-707.

DOI:

10.1115/1.2181999

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Secondary Flows and Loss Caused by Blade Row Interaction in a Turbine Stage

Authors:

Graham Pullan; Neil W. Harvey

Publication:

J. Turbomach. 2004; 128(3):484-491.

DOI:

doi: 10.1115/1.2182001

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