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Advances in Aerodynamics
Fig. 4 | Advances in Aerodynamics

Fig. 4

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

Fig. 4

① Static pressure tap; ② Location of the strain-type pressure sensor; ③ Connection line of the strong type pressure sensor; ④ Connection line for static pressure measurement at injection; ⑤ Power supply line of induced fan. ⑥ Lower part of airfoil with ducted fans; ⑦ Connection mode of airfoil and wind tunnel wall

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