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Originally posted by hesham, I've moved the pictures and added the patent
drawing from http://www.freepatentsonline.com/2288501.pdf.
It would be interesting to know the aerodynamical efficiency of the lower wing, when in the
biplane configuration, as the recess for the upper wing was fully exposed to the slipstream.
drawing from http://www.freepatentsonline.com/2288501.pdf.
It would be interesting to know the aerodynamical efficiency of the lower wing, when in the
biplane configuration, as the recess for the upper wing was fully exposed to the slipstream.