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Interference of Wing and Fuselage from Tests of 28 Combinations in the NACA Variable-Density Tunnel (1937)
NASA Technical Reports Server (NTRS) · leaf 6
3 INTERFERENCE OF WING AND FUSELAGE .12 .11 .09 \ -Combination 230 .1 II 1 I ■08% o o .06 i> .05 5 U .0,? .0/ 0§d < u .c £ o .2 .4 .6 .8 1.0 A .6 .8 1.0 LZ -.2 0. o Lift coefficient, CL Lift coefficient, CL Figure 6 —Effect of fillets on tapered-wing\ round-fuselage combinations; Figure 5.—Effect… … Lift coefficient, CL Figure 7.—Characteristics of cowled-engine, filleted combinations: kfc=Q.NASA Technical Reports Server (NTRS)
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