scholarly journals John Frederick Clarke. 1 May 1927 — 11 June 2013

2014 ◽  
Vol 60 ◽  
pp. 87-106
Author(s):  
K. N. C. Bray ◽  
N. Riley

Flying, and an enthusiasm for aviation, motivated John Clarke’s early career choices: he flew Fairey Fireflys in the Fleet Air Arm, worked in the Gas Turbine Division of Armstrong Siddeley Motors, and studied aeronautical engineering at Queen Mary College, where he graduated with first-class honours. He stayed on there to do a PhD, and then worked at English Electric, before moving to Cranfield in 1958. John Clarke’s many important publications, mainly in the general area of chemically reacting flows, cover a wide range of topics including flames, ignition processes, shock waves and detonations, the dynamics and physics of burning gases and internal ballistics, to name but a few. In all of his contributions to his subject it is perhaps too easy to overlook the individual. He had a delightful sense of humour, wore his distinctions lightly and was a most generous and friendly man.

10.2514/3.261 ◽  
1991 ◽  
Vol 5 (3) ◽  
pp. 274-283 ◽  
Author(s):  
Philip E. Buelow ◽  
John C. Tannehill ◽  
John O. levalts ◽  
Scott L. Lawrence

10.2514/3.157 ◽  
1990 ◽  
Vol 4 (2) ◽  
pp. 149-156 ◽  
Author(s):  
John C. Tannehill ◽  
John O. Ievalts ◽  
Philip E. Buelow ◽  
Dinesh K. Prabhu ◽  
Scott L. Lawrence

Author(s):  
Alexander M. Molchanov ◽  
Anna A. Arsentyeva

An implicit fully coupled numerical method for modeling of chemically reacting flows is presented. Favre averaged Navier-Stokes equations of multi-component gas mixture with nonequilibrium chemical reactions using Arrhenius chemistry are applied. A special method of splitting convective fluxes is introduced. This method allows for using spatially second-order approximation in the main flow region and of first-order approximation in regions with discontinuities. To consider the effects of high-speed compressibility on turbulence the author suggests a correction for the model, which is linearly dependent on Mach turbulent number. For the validation of the code the described numerical procedures are applied to a series of flow and heat and mass transfer problems. These include supersonic combustion of hydrogen in a vitiated air, chemically reacting flow through fluid rocket nozzle, afterburning of fluid and solid rocket plumes, fluid dynamics and convective heat transfer in convergent-divergent nozzle. Comparison of the simulation with available experimental data showed a good agreement for the above problems.


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