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Application of transition modelling in CFD for use with turbine blades
Dunn, Dwain I
;
Snedden, Glen C
;
Roos, T
;
Hildebrandt, T
(
American Institute of Aeronautics and Astronautics
,
2011-09
)
Three-component particle image velocimetry in a generic can-type gas turbine combustor
Meyers, Bronwyn C
;
Snedden, Glen C
;
Meyer, JP
;
Roos, TH
;
Mahmood, GI
(
SAGE Publications
,
2012-11
)
The design of a kerosene turbopump for a South African commercial launch vehicle
Snedden, Glen C
;
Smyth, J
;
Bindon, J
;
Brooks, M
;
Smith, G
(
AIAA 2012
,
2012-08
)
Characterisation of a refurbished 1½ stage turbine test rig for flowfield mapping behind blading with non-axisymmetric contoured endwalls
Snedden, Glen C
;
Roos, TH
;
Dunn, Dwain I
;
Gregory-Smith, D
(
American Institute of Aeronautics and Astronautics
,
2007-09
)
Turbulence model comparisons for a low pressure 1.5 stage test turbine
Dunn, Dwain I
;
Snedden, Glen C
;
Von Backström, TW
(
2009-09
)
Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor
Meyers, BC
;
Snedden, Glen C
;
Meyers, Bronwyn C
;
Roos, TH
;
Mahmood, GI
(
American Institute of Aeronautics and Astronautics
,
2009-09
)
An overview of the turbopump development programme in the University of KwaZulu-Natal’s aerospace systems research group
Smyth, J
;
Philogene, L
;
Bindon, J
;
Brooks, M
;
Smith, G
;
Snedden, Glen C
(
2012-10
)
Optimisation of non-axisymmetric end wall contours for the rotor of a low speed, 1 1/2 stage research turbine with unshrouded blades
Bergh, J
;
Snedden, Glen C
;
Meyer, C
(
ASME publications
,
2012-06
)
The development of an air injection system for the forced response testing of axial compressors
Wegman, Erik J
;
Snedden, Glen C
;
Holzinger, F
;
Schiffer, HP
;
Van der Spuy, SJ
;
Mårtensson, H
;
Ostlund, J
(
ASME
,
2013-06
)
Wave aberrations in a spinning pipe gas lens
Mafusire, C
;
Forbes, A
;
Michaelis, MM
;
Snedden, Glen C
(
2009-06
)
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