Professor Roderick Galbraith

Honorary Senior Research Fellow (School of Engineering)

email: Roderick.Galbraith@glasgow.ac.uk

R721 Level 7, Aerospace Sciences, James Watt Building South, Glasgow G12 8QQ

Publications

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Jump to: 2016 | 2010 | 2009 | 2008 | 2007 | 2006 | 2005 | 2004 | 2003 | 2002 | 2001 | 1998 | 1996 | 1995 | 1994 | 1993 | 1992 | 1989 | 1987 | 1986 | 1985 | 1984 | 1982 | 1977

Number of items: 69.

2016

Mat, S. B., Green, R. , Galbraith, R. and Coton, F. (2016) The effect of edge profile on delta wing flow. Journal of Aerospace Engineering, 230(7), pp. 1252-1262. (doi: 10.1177/0954410015606939)

2010

Sheng, W., Galbraith, R. and Chan, W. (2010) Advancement of aerofoil section dynamic stall synthesis methods for rotor design. In: Heli Japan 2010: Advanced Rotor Technology and Safety Operations, Saitama, Japan, 1-3 Nov 2010,

Sheng, W., Galbraith, R.A.M. and Coton, F.N. (2010) Applications of low speed dynamic stall model to the NREL airfoils. Journal of Solar Energy Engineering, 132(1), 011006-1-011006-8. (doi: 10.1115/1.4000329)

2009

Coton, F., Mat, S., Galbraith, R. and Gilmour, R. (2009) The effect of leading edge radius on a 65 degree delta wing. In: 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, USA, 5 - 8 January 2009,

Sheng, W., Galbraith, R. and Coton, F. (2009) On the S809 airfoil's unsteady aerodynamics characteristics. Wind Energy, 12(8), pp. 752-767. (doi: 10.1002/we.331)

2008

Sheng, W., Galbraith, R. A. M. and Coton, F. N. (2008) Prediction of dynamic stall onset for oscillatory low speed aerofoils. Journal of Fluids Engineering, 130(10), 101204. (doi: 10.1115/1.2969450)

Patek, Z., Smrcek, L. and Galbraith, R. (2008) Performance degradation of a simulated ice contaminated airfoil by super-cooled droplets. In: International Congress of the Aeronautical Sciences (ICAS), Anchorage, USA, 14-19 Sep 2008,

Sheng, W., Galbraith, R. A. and Coton, F. N. (2008) A modified dynamic stall model for low mach numbers. Journal of Solar Energy Engineering, 130(3), 031013-1. (doi: 10.1115/1.2931509)

Brown, R., Fletcher, T., Galbraith, R. and York, C. (2008) High Specification Offshore Blades: Work Package: 1B: Blades Design. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Coton, F.N., Mat, S.B., Galbraith, R.A.M. and Gilmour, R. (2008) Low speed wind tunnel characterization of the VFE-2 wing. In: 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 7th - 10th January 2008,

Sheng, W., Galbraith, R. and Coton, F. (2008) Application of a low-speed dynamic stall model to the NREL airfoils. In: 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 7 - 10 Jan 2008,

2007

Spentzos, A., Barakos, G. N. , Badcock, K. J., Richards, B. E., Coton, F. N., Galbraith, R. A. M., Berton, E. and Favier, D. (2007) Computational fluid dynamics study of three-dimensional, dynamic stall of various planform shapes. Journal of Aircraft, 44(4), pp. 1118-1128. (doi: 10.2514/1.24331)

Sheng, W., Galbraith, R. A. and Coton, F. N. (2007) Improved dynamic-stall-onset criterion at low Mach numbers. Journal of Aircraft, 44(3), pp. 1049-1052. (doi: 10.2514/1.29163)

Galbraith, R. (2007) Return from Airfoil Stall During Ramp-Down Pitching Motions. Journal of Aircraft, 44(6), pp. 1856-1864. (doi: 10.2514/1.30554)

2006

Sheng, W., Galbraith, R.A.M. and Coton, F.N. (2006) A new stall-onset criterion for low speed dynamic-stall. Journal of Solar Energy Engineering, 128(4), pp. 461-471. (doi: 10.1115/1.2346703)

Singh, C., Peake, D., Kokkalis, A., Khodagolian, V., Coton, F. and Galbraith, R. (2006) Control of rotorcraft retreating blade stall using air-set vortex generators. Journal of Aircraft, 43, pp. 1169-1176.

2005

Thomson, D.G. , Coton, F. and Galbraith, R. (2005) A simulation study of helicopter ship landing procedures incorporating measured flow-field data. Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, 219, pp. 411-427. (doi: 10.1243/095441.005X30351)

2004

Coton, F.N., Galbraith, R., Wang, T. and Newman, S. (2004) A wind-tunnel based study of helicopter tail rotor blade vortex interaction. Aeronautical Journal, 108, pp. 237-244.

Galbraith, R.A.M. (2004) Two Hundred Years of Aviation. In: Transactions of the IESIS, Glasgow, pp. 1-17.

Munduate, X., Coton, F.N. and Galbraith, R.A.M. (2004) An investigation of the aerodynamic response of a wind turbine blade to tower shadow. Journal of Solar Energy Engineering, 126, pp. 1034-1040. (doi: 10.1115/1.1765683)

2003

Cameron, D., Galbraith, R.A. and Thomson, D.G. (2003) From Pilcher to the Planets. University of Glasgow: Glasgow, UK. ISBN 085216778X

Coton, F.N. and Galbraith, R.A.M. (2003) An Examination of Dynamic Stall on an Oscillating Rectangular Wing. In: 21st AIAA Applied Aerodynamics Conference, Orlando, Florida, USA, pp. 1-8.

Ferrecchia, A., Coton, F., Galbraith, R. and Green, R. (2003) An investigation of dynamic stall onset on a pitching wing. Aeronautical Journal, 107, pp. 487-494.

2002

Fleming, A., Campbell, T., and Galbraith, R.A.M. (2002) The Simulation of Underhood Thermal Management Systems. In: Testing Expo, Stuttgart, pp. 1-7.

Galbraith, R. (2002) An Examination of Key Aerodynamic Modelling Issues Raised by the NREL Blind Comparison. Wind Energy, 5(02-Mar), pp. 199-212.

Sheng, W., Campbell, T. and Galbraith, R.A.M. (2002) The Application of CFD to Wind Tunnel Testing of Vehicles. In: Testing Expo, Stuttgart, pp. 1-13.

Wang, T., Doolan, C., Coton, F. and Galbraith, R. (2002) Experimental study of the three dimensionality of orthogonal blade-vortex interaction. AIAA Journal, 40, pp. 2037-2046.

2001

Coton, F., Galbraith, R. and Green, R. (2001) The effect of wing planform shape on dynamic stall. Aeronautical Journal, 105, pp. 151-159.

Doolan, C., Coton, F. and Galbraith, R. (2001) The effect of a preceding blade on the orthogonal vortex interaction. Journal of the American Helicopter Society, 46, pp. 221-227.

Doolan, C., Coton, F. and Galbraith, R. (2001) Surface pressure measurements of the orthogonal vortex interaction. AIAA Journal, 39, pp. 88-95.

1998

Galbraith, R.A.M., Coton, F.N., Green, R.B. and Masson, C.A. (1998) Blade Vortex Interaction Studies. Department of Aerospace Engineering report 9803. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Coton, F.N., Galbraith, R.A.M. and Copland, C.M. (1998) A Feasibility Study into the Generation of Transverse and Longitudinal Vortices in Low Speed Wind Tunnels. Internal Report 9828. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Galbraith, R.A.M., Coton, F.N. and Grant, I. (1998) An Experimental and Numerical Study to Validate an Aerodynamic Model of Yawed Flow Over a Wind Turbine. Internal Report Number 9825. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1996

Anderson, J., Galbraith, R.A.M., Green, R. and Vezza, M. (1996) The Horn, Polkemmet: Experimental Assessment of the Aerodynamic Response Characteristics. G.U. Aero Report 9609. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Copland, C.M., Coton, F.N. and Galbraith, R.A.M. (1996) Use of a Numerical Model in the Conceptual Design of a New Blade Vortex Interaction Facility. Department of Aerospace Engineering internal report no. 9509. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1995

Galbraith, R.A.M., Coton, F.N. and Jiang, D. (1995) An Investigation of Three-Dimensional Dynamic Stall. G.U. Aero Report 9542. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Galbraith, R.A.M., Coton, F.N., Vezza, M. and Robinson, D.J. (1995) A Prescribed Wake Model for Horizontal Axis Wind Turbine Incorporating Yaw and Dynamic Inflow. G.U. Aero Report 9543. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Galbraith, R.A.M., Anderson, J. and Vezza, M. (1995) A Review of the Susceptibility of the Scalpay Bridge to Aerodynamic Effects. G.U. Aero Report 9512. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1994

Green, R.B. , Galbraith, R.A.M. and Coton, F.N. (1994) An Investigation of Re-Establishment of Fully Attached Aerofoil Flow from Stall in Unsteady Conditions. G.U. Aero Report 9431. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Robison, D.J., Coton, F.N., Galbraith, R.A.M. and Vezza, M. (1994) The Development of a Prescribed Wake Model for the Prediction of the Aerodynamic Performance of Horizontal Axis Wind Turbines in Steady Axial Flow. Departmental report no. 9403. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1993

Vezza, M. , Coton, F.N. and Galbraith, R.A.M. (1993) Wind Tunnel Investigations into the Air Flow around the Existing and Proposed Bridges at Kingston. G.U. Aero Report 9316. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1992

Galbraith, R.A.M., Coton, F.N. and Jiang, D. (1992) Aerodynamic Design of Vertical Axis Wind Turbines. G.U. Aero Report 9246. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Galbraith, R.A.M., Gracey, M.W. and Leitch, E. (1992) Summary of Pressure Data for Thirteen Aerofoils on the University of Glasgow's Aerofoil Database. G.U. Aero Report 9221. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Niven, A.J., Gracey, M.W. and Galbraith, R.A.M. (1992) Collected Data for Tests on a NACA 23012A Aerofoil. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Dachun, J., Galbraith, R.A.M., Coton, F.N. and Gilmour, R. (1992) Collected Data for Tests on an AHAVAW Aerofoil. Volume I: Pressure Data from Ramp Function Tests. G.U. Aero Report 9212. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Dachun, J., Galbraith, R.A.M., Coton, F.N., Gracey, M.W. and Gilmour, R. (1992) Collected Data for Tests on an AHAVAW Aerofoil. Volume II: Pressure Data from Oscillatory Tests. G.U. Aero Report 9213. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Dachun, J., Galbraith, R.A.M., Coton, F. N., Gracey, M.W. and Gilmour, R. (1992) Collected Data for Tests on an AHAVAW Aerofoil. Volume III: Pressure Data Relevant to the Study of Large-scale Vertical-axis Wind-Turbines. G.U. Aero Report 9214. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Dachun, J., Galbraith, R.A.M., Gracey, M.W. and Gilmour, R. (1992) Collected Data for Tests on a GUVA10 Aerofoil. Volume I: Pressure Data from Ramp Function Tests. G.U. Aero Report 9217. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Dachun, J., Galbraith, R.A.M., Gracey, M.W. and Gilmour, R. (1992) Collected Data for Tests on a GUVA10 Aerofoil. Volume II: Pressure Data from Oscillatory Tests. G.U. Aero Report 9218. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Dachun, J., Galbraith, R.A.M., Gracey, M.W. and Gilmour, R. (1992) Collected Data for Tests on a GUVA10 Aerofoil. Volume III: Pressure Data Relevant to the Study of Large-scale Vertical-axis Wind-Turbines. G.U. Aero report no 9219. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Galbraith, R. A. M., Dachun, J., Green, R. B. , Gracey, M.W. and Gilmour, R. (1992) Collected Data for Tests on NACA 0015 Aerofoil with Chord of Length 0.275m. G.U. Aero Report 9209. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Galbraith, R.A.M., Gracey, M.W. and Gilmour, R. (1992) Collected Data for Tests on a NACA 0012 Aerofoil. Volume I: Pressure Data from Ramp Function Tests. G.U. Aero Report 9207. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Galbraith, R. A. M., Gracey, M.W. and Leitch, E. (1992) Contract Report for The Science And Engineering Research Council. Contract Number Gr/F/06760. G.U. Aero Report 9201. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1989

Gracey, M.W. and Galbraith, R.A.M. (1989) Data for a NACA 23012C Aerofoil Pitched about its Quarter Chord Axis. Volume II: Pressure Data from Oscillatory Tests. G.U. Aero report 8902. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Gracey, M.W. and Galbraith, R.A.M. (1989) Data for a NACA 23012C Aerofoil Pitched about its Quarter Chord Axis. Volume I: Pressure data from static and ramp function tests, with photographs of oil-flow visualisation tests. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1987

Coton, F.N. and Galbraith, R.A.M. (1987) A Direct Viscid-Inviscid Interaction Scheme for the Prediction of 2-Dimensional Aerofoil Performance in Incompressible Flow. G.U. Aero Report 8701. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

1986

Leishman, J.G., Seto, L.Y. and Galbraith, R.A.M. (1986) Collected Data for Oscillatory Pitch Tests on a NACA 23012 Aerofoil. Volume 1: Description and Pressure Data for a Reynolds Number 1.0 Million. G.U. Aero Report 8600. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

Leishman, J.G., Seto, L.Y. and Galbraith, R.A.M. (1986) Collected Data for Sinusoidal Tests on a NACA 23012 Aerofoil. Volume 2: Pressure Data for a Reynolds Number of 1.5 Million. G.U. Aero Report 8600. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

1985

Leishman, J.G. and Galbraith, R.A.M. (1985) An Algorithm for the Calculation of the Potential Flow about an Arbitrary Two Dimensional Aerofoil. G.U. Aero Report 8502. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

Galbraith, R.A.M. (1985) Comments on the Prediction of Dynamic Stall. G.U. Aero Report 8501. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

1984

Niven, A.J. and Galbraith, R.A.M. (1984) An Investigation into the Three-Dimensional Stall Development on a Modified NACA 23012 Aerofoil. G.U. Aero Report 8414. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

Seto, L.Y. and Galbraith, R.A.M. (1984) The Collected Data for Ramp Function Tests on a NACA 23012 Aerofoil. Volume 1: Description and Pressure Data. G.U. Aero Report 8413. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

Vezza, M. and Galbraith, R.A.M. (1984) Modelling of Unsteady, Incompressible Separation on an Aerofoil Using an Inviscid Flow Algorithm. G.U. Aero Report 8412. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

Galbraith, R.A.M. (1984) The Aerodynamic Characteristics of a GU25-5(11)8 Aerofoil for Low Reynolds' Numbers. G.U. Aero Report 8410. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

Niven, A.J. and Galbraith, R.A.M. (1984) A Design Procedure to Modify the Trailing Edge Upper Surface Pressure Gradient of a Given Aerofoil. G.U. Aero Report 8408. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

Vezza, M. and Galbraith, R.A.M. (1984) A Method for Predicting Unsteady Potential Flow About an Aerofoil. G.U. Aero Report 8401. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

1982

Galbraith, R.A.M. (1982) An Aspect of Aerofoil Lift and Pressure Distribution: Lecture Given to the Glasgow University Maclaurin Society on 17th November, 1982. G.U. Aero Report 8207. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

Leishman, J.G., Hanna, J. and Galbraith, R.A.M. (1982) Modelling of Trailing Edge Separation on Arbitary Two-Dimensional Aerofoils in Incompressible Flow Using an Inviscid Flow Algorithm. G.U. Aero Report 8202. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

1977

Galbraith, R.A.M. (1977) The Prediction of Turbulent Boundary Layers. G.U. Aero Report 7702. Technical Report. Department of Aeronautics and Fluid Mechanics, University of Glasgow.

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