Potential flow about arbitrary biplane wing sections
Description:
From Summary: "A rigorous treatment is given of the problem of determining the two-dimensional potential flow around arbitrary biplane cellules. The analysis involves the use of elliptic functions and is sufficiently general to include the effects of such elements as the section shapes, the chord ratio, gap, stagger, and decalage, which elements may be specified arbitrarily. The flow problem is resolved by making use of the methods of conformal representation. Thus the solution of the problem o…
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Date:
June 8, 1935
Creator:
Garrick, I. E.
Partner:
UNT Libraries Government Documents Department