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Development and application of farfield drag extraction techniques for complex viscous flows

Published online by Cambridge University Press:  04 July 2016

D. L Hunt
D. L Hunt*
Affiliation:
Aircraft Research Association (ARA), Research Department, Bedford, UK
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Abstract

A new method for deriving the components of drag from the CFD solution of an aircraft flowfield, by analysis of its wake, is presented. This method is applied to viscous flow calculations. It is also applied to configurations containing powerplants. The drag values predicted by this method are compared with the values obtained using more traditional methods, and good agreement is demonstrated.

Type
Research Article
Information
The Aeronautical Journal , Volume 105 , Issue 1045 , March 2001 , pp. 161 - 169
Copyright
Copyright © Royal Aeronautical Society 2001 

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References

1. Cumminos, R.M., Giles, M.B. and Shrinivas, G.N. Analysis of the elements of drag in three-dimensional viscous and inviscid flow, AIAA 96-2482, 1996.Google Scholar
2. Giles, M.B. and Cummings, R.M. Wake integration for three dimensional flowfield computations: theoretical development, J Aircr, March-April 1999,36,(2).Google Scholar
3. HuntD,L. D,L., Cummlngs, R.M. and Giles, M.B. Determination of drag from three-dimensional viscous and inviscid flowfield computations, AIAA 97-2257, 1997.Google Scholar
4. Hunt, D.L., Cummings, R.M. and Giles, M.B. Wake integration for three-dimensional flowfield computations: applications, J Aircr, March-April 1999,36,(2).Google Scholar
5. Schmitt, V. and Destarac, D. Recent progress in drag prediction and reduction for civil transport aircraft, at ONERA, AIAA 98-0137, 1998.Google Scholar
6. Stanniland, D.R. A selection of experimental lestcases for validation of CFD codes-Case B3,AGARD AR303, August 1994.Google Scholar
7. Private Communication, Rolls-Royce Airlines, 1998.Google Scholar
8. Shaw, J.A., Peace, A.J., Georgala, J.M. and Childs, P.N. Validation and evaluation of the advanced aeronautical CFD system SAUNA - a method developer's view, European forum in recent development and application in aeronautical CFD, 1993, Bristol, UK.Google Scholar
9. Shaw, J.A., Peace, A.J., May, N.E. and Pocock, M.K. Verification of the CFD simulation system SAUNA for complex aircraft configurations, AIAA 94-0393, 1994.Google Scholar
10. Menter, F.R. Zonal two-equation turbulence models for aerodynamic flows, AIAA 93-2906, 1993.Google Scholar