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Relative loading on biplane wings of unequal chords
It is shown that the lift distribution for a biplane with unequal chords may be calculated by the method developed in NACA Technical report no. 458 if corrections are made for the inequality in chord lengths. The method is applied to four cases in which the upper chord was greater than the lower and good agreement is obtained between observed and calculated lift coefficients.
Date:
May 18, 1934
Creator:
Diehl, Walter S.
System:
The UNT Digital Library