on differential evolution was used for optimization of the model. The results obtained from the optimization eliminated the separation experienced by the clean geometry (from 11.1% to 0%), whilst reducing the drag obtained from the best Latin Hypercube sample by 7%.
|Title of host publication||54th AIAA Aerospace Sciences Meeting|
|Publisher||American Institute of Aeronautics and Astronautics Inc. (AIAA)|
|Number of pages||19|
|Publication status||Published - 4 Jan 2016|
|Event||54th AIAA Aerospace Sciences Meeting, 2016 - San Diego, United States|
Duration: 4 Jan 2016 → 8 Jan 2016
|Conference||54th AIAA Aerospace Sciences Meeting, 2016|
|Period||4/01/16 → 8/01/16|
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Polly E Eccleston (Other), Simon H Atack (Other) & D A G Williams (Manager)