Pressure Distribution Tests on a Series of Clark Y Biplane Cellules with Special Reference to Stability (1933)
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ing istics of the orthogonal biplane. However, increasing one wing sweptback a certain amount alone or having the stagger to 50 per cent reduces maximum instability the same degree of sweepback and having sufficient by more than one-half. The range of instability is stagger to make the wing tips… … cC decalage and +50 per cent stagger cause CN maxi- pb mum of both wings to occur at virtually the same angle. Figure 46.—Effect of overhang on rolling moment due to roll at 2^=0.0.r) This condition was excellent from the standpoint of small biplane interference, but coincidence of maxi- Overhang…
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