Derivation of charts for determining the horizontal tail load variation with any elevator motion
Description:
Report presenting equations relating the wing and tail loads are derived for a unit elevator displacement. The equations are converted into a nondimensoinal form and charts are given that can be used to predict wing- and tail-load-increment variation for any type of elevator motion and for degrees of airplane stability.
Date:
January 1943
Creator:
Pearson, Henry A.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department