Relative loading on biplane wings of unequal chords (1935)
NASA Technical Reports Server (NTRS) · leaf 3
overhang. Upper wing: span bv = Z6 inches, chord cy = 6 The actual value of the effect of overhang which may inches be denoted by was not directly determined. Since Lower wing: span &x,=24 inches, chord Cr,=4 Km is subjected to the same chord correction as the inches previous factors, it is… … Overhang 7. = 100 (b„-bj.)/ba 6„ > bj, •= 100 (b„- bj)/bL ba<bL. A(7ic,= -0.018 + 0.120 CL (16) Fioukb 6.—Effect of overhang on Ki for equal chords. The test data are as follows: figure 6. For any biplane the value of is obtained Angle of attack a -4.25° by Upper wing £T22 = AZ2x[^J (14) Cxa— -.122…
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