Fig. 15From: Experimental design for a novel co-flow jet airfoilThe pressure distribution on the airfoil’s upper and lower surfaces in Simulation 2. Experimental and simulation conditions: (\(M_\infty\), Re, \(T_0\), \(P_0\)) = (0.0147, \(1.33 \times 10^5\), 287.05 K, 97,820 Pa)Back to article page