Professor Frank Coton

Strategy & Resources, and Senior-Vice Principal/Deputy Vice Chancellor (Academic) (Office of the Vice Principals)

telephone: 01413304305
email: Frank.Coton@glasgow.ac.uk

The Office of Vice Principals, Level 4, Rooms 440-442, Main Building, East Quadrangle, G12 8QQ

Personal assistant: Mrs Joanne Shearer
telephone: 01413308496
email: Joanne.Shearer@glasgow.ac.uk

Publications

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Number of items: 75.

2020

Dale, Vicki ORCID: https://orcid.org/0000-0001-6623-7412, Murray, Jo-Anne ORCID: https://orcid.org/0000-0002-8501-2742, Coton, Frank, Fischbacher-Smith, Moira, Brady, Liam and Hutchins, Nigel (2020) Advance HE Scotland Thematic Series: Technology-Enhanced Learning (TEL). [Website]

2019

Prince, Simon, Green, Richard ORCID: https://orcid.org/0000-0003-1986-408X, Coton, Frank and Wang, Yaxing (2019) The effect of steady and pulsed air jet vortex generator blowing on a aerofoil section model undergoing sinusoidal pitching. Journal of the American Helicopter Society, 64(3), pp. 1-14. (doi: 10.4050/JAHS.64.032004)

2018

Green, R.B. ORCID: https://orcid.org/0000-0003-1986-408X, Prince, S.A., Wang, Y., Khodagolian, V. and Coton, F.N. (2018) Delay of dynamic stall using pulsed air-jet vortex generators. AIAA Journal, 56(5), pp. 2070-2074. (doi: 10.2514/1.J056560)

2016

Mat, Shabudin Bin, Green, Richard ORCID: https://orcid.org/0000-0003-1986-408X, Galbraith, Roderick and Coton, Frank (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.A.McD. 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)

Gillies, E., Green, R. ORCID: https://orcid.org/0000-0003-1986-408X, Wang, Y. and Coton, F. (2010) Trailing edge flap flow control for dynamic stall. In: AHS Aeromechanics Specialists Conference, San Francisco, USA, 20-22 January 2010, (doi: 10.2514/1.17263)

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. McD. 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)

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)

Breton, S.P., Coton, F.N. and Moe, G. (2008) A study on rotational effects and different stall delay models using a prescribed wake vortex scheme and NREL phase VI experiment data. Wind Energy, 11(5), pp. 459-482. (doi: 10.1002/we.269)

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,

Currin, H.D., Coton, F.N. and Wood, B. (2008) Dynamic Prescribed Vortex Wake Model for AERODYN/FAST. Journal of Solar Energy Engineering, 130(3), 031007-0310077. (doi: 10.1115/1.2931503)

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. ORCID: https://orcid.org/0000-0002-5029-8453, Badcock, K. J., Richards, B. E., Coton, F. N., Galbraith, R. A. McD., 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, Wanan, Galbraith, Roderic A. and Coton, Frank N. (2007) Improved dynamic-stall-onset criterion at low Mach numbers. Journal of Aircraft, 44(3), pp. 1049-1052. (doi: 10.2514/1.29163)

Breton, S.P., Coton, F.N. and Moe, G (2007) A Study On Different Stall Delay Models Using A Prescribed Wake Vortex Scheme and NREL Phase VI Experiment Data. In: European Wind Energy Conference and Exhibition, Milan, Italy,

Crichton, M.l., Czarnecka, Z, Allan, Mr, Green, R.B., Badcock, K.J., Barakos, G. ORCID: https://orcid.org/0000-0002-5029-8453 and Coton, F.N. (2007) An Experimental and Numerical Study of Side-wall Interference Effects on Delta Wing Aerodynamics. In: 2nd International Symposium on Integrating CFD and Experiments in Aerodynamics, Shrivenham, pp. 1-12.

Currin, H, Coton, F.N. and Wood, B (2007) Dynamic Prescribed Vortex Wake Model for AeroDyn. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada,

Sheng, W, Galbraith, RAM and Coton, F.N. (2007) A Modified Dynamic Stall Model for Low Mach Numbers. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada,

Sheng, W, Galbraith, RAM and Coton, F.N. (2007) On the Return from Aerofoil Stall during Ramp-Down Pitching Motions. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada,

2006

Green, R. ORCID: https://orcid.org/0000-0003-1986-408X, Coton, F. and Early, J.M. (2006) On the three-dimensional nature of the orthogonal vortex interaction. Experiments in Fluids, 41(5), pp. 749-761. (doi: 10.1007/s00348-006-0198-6)

Sheng, W., Galbraith, R.A.McD. 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. J., Kokkalis, A., Khodagolian, V., Coton, F.N. and Galbraith, R. A. M (2006) Control of rotorcraft retreating blade stall using air-jet vortex generators. Journal of Aircraft, 43(4), pp. 1169-1176.

Anderle, P, Smrcek, L and Coton, F.N. (2006) Design Instrumentation and Set-up for Experimental Investigation of Wing Tip Devices. In: 3rd International Conference on Advanced Engineering Design, Prague, Czech Republic, pp. 1-9.

Green, RB, Coton, FN and Early, JM (2006) On the three-dimensional nature of the orthogonal blade-vortex interaction. Experiments in Fluids, 41, pp. 749-761. (doi: 10.1007/s00348-006-0198-6)

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

2005

Coton, F.N., Galbraith, R.A.M and Green, R.B. (2005) Analysis of model rotor blade pressures during parallel interaction with twin vortices. Journal of Aircraft, 42(6), pp. 1553-1565.

Coton, F.N., Green, RB, Early, Jm and Price, Jl (2005) Amelioration of Blade Vortex Interaction Using Blade Tip Jets. In: 61st Annual Forum of the American Helicopter Society, Grapevine, Texas,

Crichton, M.l., Czarnecka, Z., Green, G. and Coton, F. (2005) A systematic study of side-wall interference effects on delta wing aerodynamics. In: 23rd AIAA Applied Aerodynamics Conference, Toronto,

Singh, C, Peake, D, Kokkalis, Ra, Khadogolian, V, Coton, F.N. and Galbraith, RAM (2005) Parametric study of an Air-Jet vortex generator configuration to control rotorcraft retreating blade stall. In: AIAA 43rd Aerospace Sciences Meeting, Reno, Nevada,

Suttie, D.R., Coton, F.N. and Galbraith, RAM (2005) Development of an Indicial Model of Helicopter Tail Rotor Orthogonal Blade Vortex Interaction. In: AIAA 43rd Aerospace Sciences Meeting, Reno, Nevada,

Thomson, D.G. ORCID: https://orcid.org/0000-0003-3588-5710, 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)

Thomson, D.G., Coton, F.N. and Galbraith, R.A.M. (2005) Simulation study of helicopter ship landing procedures incoporating measured flow data. Proceedings of the Institution of Mechanical Engineers Part G: Journal of Aerospace Engineering, 219(5), pp. 411-427. (doi: 10.1243/095441005X30351)

2004

Coton, F.N., Marshall, J.S., Galbraith, R.A.McD. and Green, R.B. (2004) Helicopter tail rotor orthogonal blade vortex interaction. Progress in Aerospace Sciences, 40(7), pp. 453-486. (doi: 10.1016/j.paerosci.2004.11.001)

Anderle, P, Coton, F.N., Smrcek, L and Broz, V (2004) A Wind Tunnel-Based Study of the Flowfield Behind Sailplane Winglets. In: International Congress of the Aeronautical Sciences, Yokohama, Japan, pp. 1-10.

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

Early, Jm, Green, RB and Coton, F.N. (2004) Characteristics of Tail Rotor Interactions Examined Using a Particle Image Velocimetry Technique. In: AHS 4th Decennial Specialists' Meeting on Rotorcraft Aeromechanics, San Francisco, CA, USA, pp. 1-16.

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)

Singh, C, Peake, D, Kokkalis, Ra, Galbraith, RAM, Coton, F.N. and Khadogolian, V (2004) The Application of Air Jet Vortex Generators to Suppress Flow Separation on Helicopter Rotor Aerofoil Sections under Quasi-Steady and Unsteady Conditions. In: 42nd AIAA Applied Sciences Conference, Reno, Nevada, USA, pp. 1-18.

2003

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, FN, Galbraith, RAM and Green, RB (2003) An investigation of dynamic stall onset on a pitching wing. Aeronautical Journal, 107, pp. 487-494.

Fraser, B, Coton, F.N., Green, RB, Cannon, Rm and Galbraith, RAM (2003) An Analysis of High Resolution Pressure Signals on an Oscillating Delta Wing. In: 41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA,

Singh, C, Peake, DJ, Kokkalis, A, Coton, F.N. and Galbraith, RAM (2003) Control of Flow on Helicopter Rotor Blades Under Quasi-Steady and Unsteady Conditions Using Smart Air-Jet Vortex Generators. In: 29th European Rotorcraft Forum, Friedrichshafen, Germany, pp. 1-16.

Suttie, David R. and Coton, Frank N. (2003) Analysis of Tail Rotor Orthogonal Blade Vortex Interaction. Dept Report 0301. Technical Report. Department of Aerospace Engineering, University of Glasgow.

2002

Coton, F. N. and Galbraith, RAM (2002) An Examination of Key Aerodynamic Modelling Issues Raised by the NREL Blind Comparison. In: 40th AIAA Applied Sciences Conference, Reno, NV, USA,

Coton, F.N., Galbraith, RAM, Wang, T and Newman, S (2002) Preliminary Results from a Wind Tunnel-Based Study of Tail Rotor Blade Vortex Interaction. In: 28th European Rotorcraft Forum, Bristol,

Early, JM, Green, RB and Coton, FN (2002) Flow visualisation of the orthogonal blade-vortex interaction using particle image velocimetry. Aeronautical Journal, 106, pp. 137-145.

Wang, TG, Doolan, CJ, Coton, FN and Galbraith, RAM (2002) Experimental study of the three dimensionality of orthogonal blade-vortex interaction. AIAA Journal, 40, pp. 2037-2046.

2001

Coton, F.N., Green, R.B., Early, J. and Wang, T. (2001) An Investigation of the Effect of Tip Vortex Mass Injection of Blade Vortex Interaction. In: 27th European Rotorcraft Forum, Moscow, Russia,

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

Coton, FN, Jupp, ML and Green, RB (2001) Analysis of unsteady pressure signals on a pitching delta wing. AIAA Journal, 39, pp. 1750-1757.

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

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

Wang, TG and Coton, FN (2001) A high resolution tower shadow model for downwind wind turbines. Journal of Wind Engineering and Industrial Aerodynamics, 89, pp. 873-892.

1998

Jupp, M., Coton, F. and Green, R. ORCID: https://orcid.org/0000-0003-1986-408X (1998) A Statistical Analysis of Surface Pressure Measurements with Particular Reference to Vortex Breakdown. G.U. Aero Report 9806. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Galbraith, R.A.McD., Coton, F.N., Green, R.B. ORCID: https://orcid.org/0000-0003-1986-408X 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.McD. 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.McD., 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.

1997

Jupp, M., Coton, F. and Green, R. ORCID: https://orcid.org/0000-0003-1986-408X (1997) A Preliminary Study of the Flow around a Delta Wing using High Resolution Pressure Measurements. G. U. Aero Report no. 9720. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1996

Copland, C.M., Coton, F.N. and Galbraith, R.A.McD. (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.McD., 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.McD., Coton, F.N., Vezza, M. ORCID: https://orcid.org/0000-0003-4272-2987 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.

Moir, S. and Coton, F.N. (1995) An Examination of the Dynamic Stalling of Two Wing Planforms. G.U. Aero Report 9526. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1994

Green, R.B. ORCID: https://orcid.org/0000-0003-1986-408X, Galbraith, R.A.McD. 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.McD. and Vezza, M. ORCID: https://orcid.org/0000-0003-4272-2987 (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. ORCID: https://orcid.org/0000-0003-4272-2987, 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.McD., 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.

Fletcher, R., Smrcek, L. and Coton, F.N. (1992) Development of a European Aircraft Design Consortium in Higher Education. TEMPUS Joint European Project 11 79-90/1. Final report for year 1990-1991. Departmental report no. 9223. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Fletcher, R., Smrcek, L. and Coton, F.N. (1992) Development of a European Aircraft Design Consortium in Higher Education. TEMPUS Joint European Project 11 79-91/2. Interim progress report for year 1991-1992. Departmental report no. 9224. Technical Report. Department of Aerospace Engineering, University of Glasgow.

Dachun, Jiang, Galbraith, R.A.McD., 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, Jiang, Galbraith, R.A.McD., 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, Jiang, Galbraith, R.A.McD., Coton, Frank 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.

1991

Fletcher, R., Smrcek, L. and Coton, F.N. (1991) Development of a European Aircraft Design Consortium in Higher Education. TEMPUS Joint European Project 11 79-90/1. Interim report for year 1990-1991. Departmental report no. 9222. Technical Report. Department of Aerospace Engineering, University of Glasgow.

1987

Coton, F.N. and Galbraith, R.A.McD. (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.

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