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Effect of laser shock peening on fatigue life at stress raiser regions of a high-speed micro gas turbine shaft: A simulation based study
Pretorius, JG
;
Desai, DA
;
Snedden, Glen C
(
Trans Tech Publications
,
2019-11
)
CFD analysis of the impingement cooling effect of the coolant jet caused by the T56 1st stage disc metering hole
Snedden, Glen C
;
Lambert, T
(
2003-09
)
Development of an automated non-axisymmetric endwall contour design system for the rotor of a 1-stage research turbine - Part 2 Computed and experimental results
Bergh, J
;
Snedden, Glen C
;
Reddy, D
(
Sage Journals
,
2020-01
)
Development of an automated non-axisymmetric endwall contour design system for the rotor of a 1-stage research turbine - Part 1 System Design
Bergh, J
;
Snedden, Glen C
;
Reddy, D
(
Sage Publications Ltd
,
2019-09
)
On-and off-design performance of a model rotating turbine with non-axisymmetric endwall contouring and a comparison to cascade data
Snedden, Glen C
;
Dunn, Dwain I
;
Ingram, G
(
Cambridge University Press
,
2018-04
)
Characterisation of a spinning pipe gas lens using a Shack–Hartmann wavefront sensor
Mafusire, C
;
Forbes, A
;
Snedden, Glen C
;
Michaelis, MM
(
International Society for Optical Engineering (SPIE)
,
2007
)
Computational fluid dynamics model of the spinning pipe gas lens
Mafusire, C
;
Forbes, A
;
Snedden, Glen C
(
2010-08
)
Experimental and numerical study of near bleed hole heat transfer enhancement in internal turbine blade cooling channels
Scheepers, G
;
Morris, RM
;
Visser, JA
;
Roos, TH
;
Snedden, Glen C
(
2006-01
)
Observations on the selection of objective function for the optimisation of turbine endwalls using computational fluid dynamics
Snedden, Glen C
;
Dunn, Dwain I
;
Von Backström, TW
;
Ingram, G
(
South African Conference on Computational and Applied Mechanics
,
2010-01
)
Performance of a generic non-axisymmetric end wall in a single stage, rotating turbine at on and off-design conditions
Snedden, Glen C
;
Dunn, Dwain I
;
Ingram, G
;
Gregory-Smith, D
(
2010 by ASME
,
2010-06
)
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