Relative loading on biplane wings of unequal chords (1935)
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s greater than the lower and good agreement is obtained be designated K10. It is due principally to the restric- between observed and calculated lift coefficients. tion in area which increases the velocity and decreases INTRODUCTION the static pressure between the wing3. The curve of Kio against… … .08 .12 .16 .20 .24 .04 Thickness of lower wing t wings, respectively. Ratio, Gap " <? ACLjj is given by an equation of the form Fioube 1.—Effect of wing thickness and gap on Kt at sero lift and rem stagger for equal chords. (4) curve was based on biplanes of equal chords but it where the constant…
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