This research paper shows that for a given aspect ratio and wing area, compared to a monoplane a biplane produced a better L/D. So, wouldn't it make more sense to manufacture biplanes for subsonic flight instead when size and wingspan restrictions are involved?
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If you attach a second wing to a monoplane then each wing must generate only ½ of the total lift; being the induced drag proportional to L² then each wing generates now only ¼ of induced drag; the total induced drag is therefore ¼+¼=½ of the monoplane case. Amazing result. Anyway induced drag is also inversely proportional to wingspan squared: the same reduction of ½ can be obtained simply increasing wingspan of some 40%. What's better depends on other constraints
– sophit Jun 11 '23 at 14:52