A method for computing leading-edge loads
Description:
From Summary: "In this report a formula is developed that enables the determination of the proper design load for the portion of the wing forward of the front spar. The formula is inherently rational in concept, as it takes into account the most important variables that affect the leading-edge load, although theoretical rigor has been sacrificed for simplicity and ease of application. Some empirical corrections, based on pressure distribution measurements on the PW-9 and M-3 airplanes have been…
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Date:
January 16, 1931
Creator:
Rhode, Richard V. & Pearson, Henry A.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department