An extended theory of thin airfoils and its application to the biplane problem (1931)
NASA Technical Reports Server (NTRS) · leaf 24
ual lift coefficient is the same in the biplane as in the case of a monoplane wing. The most interesting and important quantity dis- cussed in this paper is the relative lift distribution between the two wings. It has seemed of most prac- Glauert has given a very simple method of finding tical… … investigated. Fegukk 8.—K. A. F.-15 equal wing biplane X=B,^-L0, r—15.ft°. Decreasing the gap-chord ratio de- creases dCLJda as is to be expected. No decalage. Experimental data from R. & M. Kos. 857 and 810. Quantitative data on this point have upper wing to lift coefficient of the biplane" have…
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