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Results: 1
Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils
Authors:
Chen, CFA Lotz, RD Thompson, BE
Citation:
Cfa. Chen et al., Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils, COMPUT FLU, 31(1), 2002, pp. 25-40
Risultati:
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