Experimental Set-Up for 2D Cargo Release Test in Subsonic Wind Tunnel

The objective of this research is to design a 2D inexpensive mechanism for testing the cargo separation in a wind tunnel. Our designed mechanism simulates the separation of a NACA-0012 airfoil from the upper wall of a wind tunnel. To perform the test, we have used a low-speed (0–100 m/s) wind tunnel...

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