Interference of Wing and Fuselage from Tests of Eight Combinations in the NACA Variable-density Tunnelcombinations with Tapered Fillets and Straight-side Junctures (1938)
NASA Technical Reports Server (NTRS) · leaf 14
A.C.A. Teohnical Note N0. 642 Fig. 6 .10 … Figure 6. - Characteristics for low-wing combination with straight-side lunctures and horizontal tail surfaces; round fuselage, tapered N.A.C.A. 0018-09 airfoil; k/c • -0.23, lg - 0°7
NASA Technical Reports Server (NTRS)
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