Aerodynamics of slender wings and wing-body combinations having swept trailing edges
Description:
From Introduction: "In the present paper, a general method is developed for solving low-aspect-ratio problems involving shed vortex sheets. Both direct and inverse problems are considered. The method is applicable for all planar problems where the velocity boundary conditions can be made homogeneous by differentiation in either the streamwise or the spanwise directions."
Date:
March 1954
Creator:
Mirels, Harold
Item Type:
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Partner:
UNT Libraries Government Documents Department