The application of non-axisymmetric endwall contouring in a single stage, rotating turbine G Snedden, D Dunn, G Ingram, D Gregory-Smith
Turbo Expo: Power for Land, Sea, and Air 48883, 831-840, 2009
62 2009 The performance of a generic non-axisymmetric end wall in a single stage, rotating turbine at on and off-design conditions G Snedden, D Dunn, G Ingram, D Gregory-Smith
Turbo Expo: Power for Land, Sea, and Air 44021, 1069-1080, 2010
59 2010 Unsteady Effects of a Generic Non-Axisymmetric Endwall Contour on the Rotor of a 1½ Stage Low Speed Turbine Test Rig D Dunn, G Snedden, T von Backström, MP Mdluli
Turbo Expo: Power for Land, Sea, and Air 55249, V06CT42A024, 2013
17 2013 Turbulence model comparisons for a low pressure 1.5 stage test turbine DI Dunn, GC Snedden, TW Von Backström
17 2009 Optimization of Non-axisymmetric Endwall Contours for the Rotor of a Low Speed, J Bergh, G Snedden, D Dunn
Journal of turbomachinery 142 (4), 041006, 2020
14 2020 Characterisation of a refurbished 1½ stage turbine test rig for flowfield mapping behind blading with non-axisymmetric contoured endwalls GC Snedden, TH Roos, DI Dunn, D Gregory-Smith
American Institute of Aeronautics and Astronautics, 2007
14 2007 FLOW FIELDS IN AN AXIAL FLOW COMPRESSOR DURING FOUR-QUADRANT OPERATION A Gill, T von Backström, T Harms, D Dunn
Proceedings of ASME Turbo Expo 2013, 2013
13 2013 Observations on the selection of objective function for the optimisation of turbine endwalls using computational fluid dynamics GC Snedden, DI Dunn, TW Von Backström, G Ingram
South African Conference on Computational and Applied Mechanics, 2010
11 2010 Unsteady effects of a generic non-axisymmetric rotor endwall contour on a 1½ stage turbine test rig at off design conditions D Dunn, G Snedden, T von Backström
Turbo Expo: Power for Land, Sea, and Air 45639, V02DT44A009, 2014
9 2014 Experimental investigation into the unsteady effects on non-axisymmetric turbine endwall contouring DI Dunn, GC Snedden, TW Von Backström
South African Conference on Computational and Applied Mechanics, 2010
8 2010 Numerical investigation into the unsteady effects of non-axisymmetric turbine endwall contouring on secondary flows DI Dunn, TW Von Backström
American Institute of Aeronautics and Astronautics, 2011
6 2011 The effect of endwall contouring on the unsteady flow through a turbine rotor DI Dunn
Stellenbosch: Stellenbosch University, 2014
4 2014 On-and off-design performance of a model rotating turbine with non-axisymmetric endwall contouring and a comparison to cascade data G Snedden, D Dunn, G Ingram
The Aeronautical Journal 122 (1250), 646-665, 2018
3 2018 An unsteady numerical analysis of a generic non-axisymmetric turbine endwall in a 1½ stage turbine test rig D Dunn, T von Backström, G Snedden
The Aeronautical Journal 119, 2015
3 2015 The numerical investogation of a bank of delta plenum air-cooled heat exchangers DI Dunn
3 2006 Application of transition modelling in CFD for use with turbine blades DI Dunn, GC Snedden, T Roos, T Hildebrandt
American Institute of Aeronautics and Astronautics, 2011
2 2011 Unsteady Analysis of a Generic NonAxisymmetric Hub Endwall Contour as Applied to a Rotating Turbine at On and Off-Design Conditions. D Dunn, G Snedden, TW von Backström
The R&D Journal 34, 2018
2018 The effect of a hub fillet radius on a non-axisymmetric endwall contour. D Dunn, G Snedden
ISABE 2017, 2017
2017 Non-axisymmetric endwall contouring in a model rotating turbine at on and off-design speeds and a comparison to cascade data G Snedden, D Dunn, G Ingram
ISABE 2017, 2017
2017 
Glen SneddenProfessor of Aerospace Engineering, University of KwaZulu NatalDirección de correo verificada de ukzn.ac.za