Contact Professor Simon Prince
- Tel: +44 (0) 1234 750111
- Email: simon.prince@cranfield.ac.uk
- ORCID
Areas of expertise
- Computational Fluid Dynamics
- Flight Physics
Background
Graduated from University of Sheffield with a MEng(Hons) in Mechanical Engineering in 1995 before graduating from the MSc Aerodynamics course at Cranfield University the year later. Completed a PhD in high speed aerodynamics at Cranfield while working for the Defence Research Agency, where Simon worked on experimental and CFD projects ranging from missile, civil and combat aircraft aerodynamics and propulsion integration. Was at City University of London from 2004-2014, completing a MA in Academic Practice in 2010. Simon helped establish and was seconded to the UK Aerospace Technology Institute until 2017. He is secretary of the Association of Aerospace Universities, a member of the ESDU Transonics committee and the UK Vertical Lift Network.
Current activities
Experimental and Computational high speed (transonic, supersonic and hypersonic) aerodynamics.
Aerodynamic flow control.
Computational Fluid Dynamics.
Clients
- Airbus SE
- Aircraft Research Association
- Aerospace Technology Institute
- Reaction Engines Ltd
- ACCURIS (ESDU)
Publications
Articles In Journals
- Tsentis S, Goulos I, Debiasi M, Prince S, Pachidis V, .... (2025). Wind tunnel installation effects on a high-speed exhaust flow under large blockage. Journal of Spacecraft and Rockets, ahead-of-print(ahead-of-print)
- Bang CS, Rana ZA & Prince SA. (2024). CFD analysis on novel vertical axis wind turbine (VAWT). Machines, 12(11)
- Barrington J, James S, Kissinger T, Staines S, Prince S, .... (2023). Optical fibre pressure sensing using a frequency modulated laser-based signal processing technique. Measurement Science and Technology, 34(7)
- Di Pasquale D & Prince S. (2023). Passive transonic shock control on bump flow for wing buffet suppression. Aerospace, 10(6)
- Tsentis S, Goulos I, Prince S, Pachidis V & Zmijanovic V. (2023). Propulsion aerodynamics for a novel high-speed exhaust system. Journal of Engineering for Gas Turbines and Power, 145(12)
- Kshitij A, Prince SA, Stollery JL & de la P Ricón F. (2021). A simple method for drag estimation for wedge-like fairings in hypersonic flow. The Aeronautical Journal, 125(1288)
- Prince SA, Badalamenti C & Georgiev D. (2020). Experimental investigation of a variable geometry vertical axis wind turbine. Wind Engineering, 45(4)
- Prince SA, Green R, Coton F & Wang Y. (2019). The effect of steady and pulsed air jet vortex generator blowing on an aerofoil section model undergoing sinusoidal pitching. Journal of the American Helicopter Society, 64(3)
- Green RB, Prince SA, Wang Y, Khodagolian V & Coton FN. (2017). Delay of dynamic stall using pulsed air-jet vortex generators. AIAA Journal, 56(5)
- Prince SA, Badalamenti C & Regas C. (2016). The application of passive air jet vortex-generators to stall suppression on wind turbine blades. Wind Energy, 20(1)
- Prince S, Yemets V & Wilkinson R. (2015). Investigations of a Combustible Inertial Launch Vehicle Design. JBIS. Journal of the British Interplanetary Society, 67(7)
- Thouault N, Breitsamter C, Adams NA, Seifert J, Badalamenti C, .... (2012). Numerical Analysis of a Rotating Cylinder with Spanwise Disks. AIAA Journal, 50(2)
- Prince SA & Khodagolian V. (2011). Low-Speed Static Stall Suppression Using Steady and Pulsed Air-Jet Vortex Generators. AIAA Journal, 49(3)
- Prince SA & Williams MJ. (2009). Parabolized navter-stokes investigations of hypersonic intake flows. JBIS - Journal of the British Interplanetary Society, 62(3)
- Prince SA, Khodagolian V, Singh C & Kokkalis T. (2009). Aerodynamic Stall Suppression on Aerofoil Sections Using Passive Air-Jet Vortex Generators. AIAA Journal, 47(9)
- Khalid M, Dujardin A, Hennig P, Leavitt L, Leopold F, .... (2005). Turbulence Model Studies to Investigate the Aerodynamic Performance of a NASA Dual Control Missile at Supersonic Mach Numbers. Canadian Aeronautics and Space Journal, 51(4)
- Prince SA, Vannahme M & Stollery JL. (2005). Experiments on the hypersonic turbulent shock-wave/boundary-layer interaction and the effects of surface roughness. The Aeronautical Journal, 109(1094)
- Princet SA & Qin N. (2002). Mechanism of windward vortex shocks about supersonic slender bodies. The Aeronautical Journal, 106(1063)