Aeronautical Engineering/wing area

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Question

Wing Diagrams
I know that lift is related to the area of the wing, so does this mean that two wings just above (say half a foot above) would produce the same lift as one single wing with the same total area? For example (as in the attached picture), if a wing had the same total area, but was divided in two, would the lift change given identical other conditions?

Answer
Two wings far apart would produce approximately the same lift as a single wing with the same total area.  But as the two wings are brought together, they interfere with each other.  That is - the flow field of one creates a negative effect on the flow field of the other.  Two wings (aspect ratio 6) separated vertically by one chord will produce roughly only 20% more lift than a single wing of the same total area.  Two wings even closer together would have even less total lift.  In the limit, if the wings were touching it would be like a single wing with a very odd shape.

Biplanes were developed in the early days because of the strength inherent in a box structure.  Good mono structure wings were not developed yet.  The biplane also has high drag because of the guy wires, mutual interference, and low aspect ratios.  A wing with low aspect ratio has more drag than a wing with high aspect ratio as seen in modern gliders.
Paul

Paul Soderman

Expertise

Aeronautics, Fluid Mechanics, Aeroacoustics, Noise Control, Muffler Design, Wind Tunnel Research.... I know nothing about India - do not ask about schools, jobs, application requirements, career choices, etc. for India. Please, no text message verbiage; I prefer full words in full sentences. Thanks.

Experience

38 years as research engineer at NASA

Publications
AIAA, NASA

Education/Credentials
B.S. and M.S. Aeronautical Engineering - U. of Washington Graduate work Standford U.

Awards and Honors
AIAA Associate Fellow (American Institute of Aeronautics and Astronautics)

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