Showing 19 out of 51 publications matching your search
A Web-Based Database Approach to CFD Post-Processing
Authors:
Graham Pullan
Publication:
AIAA 2017-0814
DOI:
10.2514/6.2017-0814
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
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
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
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
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
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
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
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
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