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Researchspace >
Browsing by Author Snedden, GC
Showing results 1 to 12 of 12
| Issue Date | Title | Author(s) | | Sep-2003 | CFD analysis of the impingement cooling effect of the coolant jet caused by the T56 1st stage disc metering hole | Snedden, GC; Lambert, T |
| Jul-2006 | CFD model of a spinning pipe gas lens | Snedden, GC; Forbes, A; Mahlatse, ACK; Mafusire, C; Michaelis, MM |
| Sep-2007 | Characterisation of a refurbished 1½ stage turbine test rig for flowfield mapping behind blading with non-axisymmetric contoured endwalls | Snedden, GC; Roos, TH; Dunn, D; Gregory-Smith, D |
| Sep-2003 | Detailed disc assembly temperature prediction: comparison between CFD and simplified engineering methods | Snedden, GC; Roos, TH; Naidoo, K |
| Jan-2006 | 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, GC |
| Sep-2011 | Experimental results showing the internal three-component velocity field and outlet temperature contours for a model gas turbine combustor | Meyers, BC; Snedden, GC; Meyer, JP; Roos, TH; Mahmood, GI |
| Jul-2006 | Gas lensing in a heated spinning pipe | Mafusire, C; Forbes, A; Snedden, GC; Mahlase, ACK; Michaelis, MM; Mathuthu, M |
| Jun-2008 | Optical aberrations in a spinning pipe gas lens | Mafusire, C; Forbes, A; Michaelis, MM; Snedden, GC |
| Sep-2003 | Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer | Snedden, GC |
| Nov-2012 | Three-component particle image velocimetry in a generic can-type gas turbine combustor | Meyers, BC; Snedden, GC; Meyer, JP; Roos, TH; Mahmood, GI |
| Sep-2009 | Three-dimensional particle image velocimetry in a generic can-type gas turbine combustor | Meyers, BC; Snedden, GC; Meyer, JP; Roos, TH; Mahmood, GI |
| Sep-2009 | Turbulence model comparisons for a low pressure 1.5 stage test turbine | Dunn, D; Snedden, GC; Von Backström, TW |
Showing results 1 to 12 of 12
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