Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils
- 1 January 2002
- journal article
- Published by Elsevier in Computers & Fluids
- Vol. 31 (1) , 25-40
- https://doi.org/10.1016/s0045-7930(01)00014-7
Abstract
No abstract availableKeywords
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