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Experimental Determination of Jet Boundary Corrections for Airfoil Tests in Four Open Wind Tunnel Jets of Different Shapes (1931)
NASA Technical Reports Server (NTRS) · leaf 9
REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS D = 0.43Z, Streamline struts -i.oz Id Drag _ sfruC Rear lift 'and mo ~ Droq^ ment wire wire D=0.43Z A,Lug Sockel Droq ^ Note: ^ 'Drag screw pulley Dimensions in Z of yoke chord wires i)=a43z\\ Streomline strut-^\ ^ Counter weight 3 Counter weight… … Figure 8.—Circular jet with 5-inch chord airfoil set-upNASA Technical Reports Server (NTRS)
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