City Research Online

Article

Veerasamy, D., Atkin, C.J. & Ponnusami, S. A. ORCID: 0000-0002-2143-8971 (2021). Aerofoil wake-induced transition characteristics on a flat-plate boundary layer. Journal of Fluid Mechanics, 920, article number A29. doi: 10.1017/jfm.2021.452

Veerasamy, D. & Atkin, C.J. ORCID: 0000-0003-2529-1978 (2020). A rational method for determining intermittency in the transitional boundary layer. Experiments in Fluids, 61(1), article number 11. doi: 10.1007/s00348-019-2856-5

Dirks, T. B. & Atkin, C.J. ORCID: 0000-0003-2529-1978 (2019). A consolidated method for predicting laminar boundary layers on rotating axi-symmetric bodies. European Journal of Mechanics, B/Fluids, 75, pp. 271-278. doi: 10.1016/j.euromechflu.2018.10.013

Gowree, E. R., Jagadeesh, C. & Atkin, C.J. (2019). Skin friction drag reduction over staggered three dimensional cavities. Aerospace Science and Technology, 84, pp. 520-529. doi: 10.1016/j.ast.2018.11.001

Miao, X., Zhang, Q. ORCID: 0000-0003-0982-2986, Atkin, C.J. ORCID: 0000-0003-2529-1978 , Sun, Z. & Li, Y.view all authors (2018). Improving Purge Air Cooling Effectiveness by Engineered End-Wall Surface Structures-Part I: Duct Flow. Journal Of Turbomachinery, 140(9), pp. 1-12. doi: 10.1115/1.4040853

Bottemanne, M. & Atkin, C.J. (2018). Tool for sizing suction pumps for hybrid laminar flow control concepts. International Journal of Mechanical Engineering and Robotics Research, 7(1), pp. 1-8. doi: 10.18178/ijmerr.7.1.1-8

Miao, X., Zhang, Q. ORCID: 0000-0003-0982-2986, Atkin, C.J. ORCID: 0000-0003-2529-1978 , Sun, Z. & Li, Y.view all authors (2018). Improving Purge Air Cooling Effectiveness by Engineered End-Wall Surface Structures-Part II: Turbine Cascade. Journal Of Turbomachinery, 140(9), article number 091002. doi: 10.1115/1.4040854

Panagopoulos, I., Atkin, C.J. & Sikora, I. (2017). Developing a performance indicators lean-sigma framework for measuring aviation system’s safety performance. Transportation Research Procedia, 22, pp. 35-44. doi: 10.1016/j.trpro.2017.03.005

Panagopoulos, I., Atkin, C.J. & Sikora, I. (2016). Lean Six-Sigma in Aviation Safety: An implementation guide for measuring aviation system’s safety performance. Journal of Safety Studies, 2(2), doi: 10.5296/jss.v2i2.10438

Atkin, C.J. (2001). New aerodynamic approaches to suction system design. Notes on Numerical Fluid Mechanics, 76(3), pp. 55-63. doi: 10.1007/978-3-540-45359-8_7

Book Section

Crowley, B.J. & Atkin, C.J. (2016). Investigation of the discrete effects of suction in large scale arrays for Laminar flow control. In: 34th AIAA Applied Aerodynamics Conference. . Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-3117

van Bokhorst, E., Placidi, M. & Atkin, C.J. (2016). The influence of the spatial frequency content of discrete roughness distributions on the development of the crossflow instability. In: 8th AIAA Flow Control Conference. . Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-3931

Conference or Workshop Item

Fumarola, I., Gaster, M. & Atkin, C.J. (2016). Experimental investigation of the vorticity amplification on a swept wing with a blunt leading edge. Paper presented at the 52nd 3AF International Conference on Applied Aerodynamics, 27-29 Mar 2017, Lyon, France.

Corlho, L., Placidi, M., Atkin, C.J. & Sun, Z.view all authors (2016). Experimental Investigation of a Handley Page Triple Slotted Aerofoil. Paper presented at the 2016 Applied Aerodynamics Conference: Evolution & Innovation Continues - The Next 150 Years of Concepts, Design and Operations, 19-21 July 2016, Bristol, UK.

Alderman, J., Rolston, S., Gaster, M. & Atkin, C.J.view all authors (2016). A method of reducing the drag of transport wings. In: 34th AIAA Applied Aerodynamics Conference. 34th AIAA Applied Aerodynamics Conference, 13-17 June 2016, Washington D. C., USA. doi: https://arc.aiaa.org/doi/10.2514/6.2016-3115

Atkin, C.J. & Backer Dirks, T. (2015). Systems driven HLFC design. Paper presented at the 50th 3AF International Conference on Applied Aerodynamics, 30 Mar - 01 Apr 2015, Toulouse, France.

Atkin, C.J. (2014). Convergence of calculated transition loci during computational analysis of transonic aerofoils and infinite swept wings. Paper presented at the 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, 7-12 Sep 2014, St Petersburg, Russia.

Atkin, C.J. (2004). Performance trade-off studies for a retrofit Hybrid Laminar Flow Control system. Paper presented at the 2nd AIAA Flow Control Conference, 26 June - 1 July, Portland, Oregon.

Atkin, C.J. & Schrauf, G. (2000). Progress in linear stability methods for design applications. Paper presented at the European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2000), 11-14 Sep 2000, Barcelona, Spain.

Atkin, C.J. Predicting the mission performance of a retrofit Hybrid Laminar Flow Control system. Paper presented at the Aerospace Aerodynamics Research Conference, 2002.

Arthur, M.T. & Atkin, C.J. Transition modelling for viscous flow prediction.. Paper presented at the 36th AIAA Fluid Dynamics Conference and Exhibit, 5-8 June 2006, San Francisco, California.