City Research Online

Article

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

Jagadeesh, C., Gowree, E. R., Jadidbonab, H. & Atkin, C. J. ORCID: 0000-0003-2529-1978view all authors (2018). On the temporal analysis of acoustic waves using schlieren imaging. Measurement, 116, pp. 507-513. doi: 10.1016/j.measurement.2017.11.018

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

Xu, H., Mughal, S. M., Gowree, E. R. , Atkin, C. J. & Sherwin, S. J.view all authors (2017). Destabilisation and modification of Tollmien-Schlichting disturbances by a three-dimensional surface indentation. Journal of Fluid Mechanics, 819, pp. 592-620. doi: 10.1017/jfm.2017.193

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

Gowree, E. R. & Atkin, C. J. (2017). Measurement and modelling of the turbulent boundary layer near the attachment line of a swept wing. Aeronautical Journal, 121(1240), pp. 746-769. doi: 10.1017/aer.2017.30

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

Gowree, E. R., Atkin, C. J. & Gruppetta, S. (2015). A simple digital-optical system to improve accuracy of hot-wire measurements. MEASUREMENT SCIENCE and TECHNOLOGY, 26(9), article number 095303. doi: 10.1088/0957-0233/26/9/095303

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

Placidi, M., van Bokhorst, E. & Atkin, C. J. (2016). On the effect of discrete roughness on the growth of crossflow instability in very low turbulence environment. In: 8th AIAA Flow Control Conference. . Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2016-3470

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

Atkin, C. J. & Gowree, E. R. (2016). Staggered Three-dimensional Cavities as a Possible Method for Skin Friction Drag Reduction. In: Proceedings of the 30th International Council of the Aeronautical Sciences. . Bonn, Austria: The International Council of the Aeronautical Sciences.

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.

Gowree, E. R. & Atkin, C. J. (2016). On the excitation of Tollmien-Schlichting waves due to surface vibration. 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

Jagadeesh, C., Gowree, E. R. & Atkin, C. J. (2015). Development of a quantitative Schlieren imaging technicque for acoustic waves. Paper presented at the 51st 3AF International Conference on Applied Aerodynamics, 4-6 Apr 2016, Strasbourg, France.

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.

Gowree, E. R. & Atkin, C. J. (2015). On the turbulent mean-flow at the leading edge of a swept wing. 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.

Gowree, E. R. & Atkin, C. J. (2014). Incompressible turbulent flow at the leading edge of swept wings. In: 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014. 29th Congress of the International Council of the Aeronautical Sciences, 7-12 Sep 2014, St Petersburg, Russia.

Atkin, C. J. & Gowree, E. R. (2012). Recent Developlments to the viscous Garabedian and Korn method. Paper presented at the 28th Congress of the International Council of the Aeronautical Sciences, 23-28 Sep 2012, Brisbane, Australia.

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.