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A Method for Computing Leading-Edge Loads (1933)

NASA Technical Reports Server (NTRS) · leaf 4

An illustration from A Method for Computing Leading-Edge Loads, 1933, leaf 4
nes at high angles of attack and in nose the wing forward of the front spar. The formula is inher- dives have indicated the necessity for a revision of the ently rational in concept, as it takes into account the specifications for the design of the leading edge of the most important variables that… … Figure I.—Leading-edge failure that occurred in a fast dive good criterion for the strength of the leading-edge struc- and ease of application. Some empirical corrections, ture in the high angle of attack condition, the entirely based on pressure distribution measurements on the arbitrary provision…

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