Gonzalez, Feli - QUT ePrints

UpLower. SCB. 0.0129 0.0106 2.23×10-3. 13.587. Optimum. Aerofoil. 0.0102 0.0091 1.06×10-3. 17.207. Figure 28. Drag comparison at increasing Cl. [M 0.8, Re 18.63 ...

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