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Advances in Aerodynamics
Fig. 10 | Advances in Aerodynamics

Fig. 10

From: Experimental design for a novel co-flow jet airfoil

Fig. 10

Variation of the lift coefficient of the OCFJ airfoil with angles of attack in wind tunnel experiments and numerical simulations. Exp. stands for experiment results and Sim. is simulation results. Experimental and simulation conditions: (\(M_\infty\), Re, \(T_0\), \(P_0\)) = (0.0147, \(1.33 \times 10^5\), 287.05 K, 97,820 Pa)

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