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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 21
Note No. 641 Fig. 6 N.A.C.A. Technical … -4 0 4 8 18 16 80 24 28 32 Angle of attack, a , deg. Figure 6. - Effect of special leading-edge fillete on the interference burble. Rectangular N.A.C.A. 0012 airfoil and round fuselage. Midwing position.NASA Technical Reports Server (NTRS)
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