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A Method for Computing Leading-Edge Loads (1933)

NASA Technical Reports Server (NTRS) · leaf 5

An illustration from A Method for Computing Leading-Edge Loads, 1933, leaf 5
er, and that the dis- although, in keeping with the interests of the practical tribution of the additional load is the same for any air- designer, liberties have been taken with the rigorous foil except for a narrow region near the leading edge theory to simplify the result as much as possible con-… … FlGTTBE 2—Result of leading-edge failure. Air entering at the opening of the seam burst the fabric Neglecting the minor variations at the nose, we may il has been adjusted to give the best accuracy in the write, with only small error, for the whole wing section. critical loading conditions. The…

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