Publications

A Web-Based Database Approach to CFD Post-Processing

Authors:

Graham Pullan

Publication:

AIAA 2017-0814

DOI:

10.2514/6.2017-0814

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Modeling Nonuniform Bleed in Axial Compressors

Authors:

Grimshaw, S.D., Pullan, G. and Hynes, T.P.

Publication:

Journal of Turbomachinery (2016) Vol. 138, Issue 9, Article 091010

DOI:

10.1115/1.4032845

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Bleed Induced Distortion in Axial Compressors

Authors:

Grimshaw, S.D., Pullan, G. and Walker, T.

Publication:

Journal of Turbomachinery (2015) Vol. 137, Issue 9, Article 101009

DOI:

10.1115/1.4030809

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Origins and Structure of Spike-Type Rotating Stall

Authors:

Pullan, G., Young, A.M., Day, I.J., Greitzer, E.M. and Spakovszky, Z.S.

Publication:

J. Turbomach 137(5), 051007 (May 01, 2015) (11 pages)

DOI:

10.1115/1.4028494

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Aerodynamic Design of High End Wall Angle Turbine Stages—Part II: Experimental Verification

Authors:

A. W. Cranstone; G. Pullan; E. M. Curtis; S. Bather

Publication:

J. Turbomach. 2013; 136(2):021007-021007-10.

DOI:

10.1115/1.4023906

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Improving Intermediate Pressure Turbine Performance by Using a Nonorthogonal Stator

Authors:

Sungho Yoon; John Denton; Eric Curtis; John Longley; Graham Pullan

Publication:

J. Turbomach. 2013; 136(2):021012-021012-8.

DOI:

10.1115/1.4023941

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Aerodynamic Design of High End Wall Angle Turbine Stages—Part I: Methodology Development

Authors:

A. W. Cranstone; G. Pullan; E. M. Curtis; S. Bather

Publication:

J. Turbomach. 2013; 136(2):021006-021006-8.

DOI:

10.1115/1.4023905

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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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