The aerodynamic characteristics at transonic speeds of an all-movable, tapered, 45 degrees sweptback, aspect-ratio-4 tail surface deflected about a skewed hinge axis
Description:
From Introduction: "The purpose of the present paper was to determine whether the characteristics about a skewed axis could be predicted from data about the normal angle-of-attack axis, and whether such a configuration offered any aerodynamic advantages over the conventional hinge location normal to the pane of symmetry."
Date:
July 3, 1952
Creator:
Hammond, Alexander D. & Watson, James M.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department