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Interference of Wing and Fuselage from Tests of 17 Combinations in the NACA Variable-density Tunnel Combination with Special Junctures (1938)
NASA Technical Reports Server (NTRS) · leaf 20
N.A.C.A. Technical Note No. 641 Fig. 5 … Figure 5. - Effect of surface finish at junctures of a critical wing-fuselage combination. Rectangular N.A.C.A. 0013 airfoil and round fuselage with tapered fillets. Midwing position.NASA Technical Reports Server (NTRS)
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