Additional design charts relating to the stalling of tapered wings
Description:
From Introduction: "The present report, therefore, may be considered a supplement to reference 1. The combined scope of the stall charts of reference 1, designated A, and of the present work, designated B, is summarized in the following table: For the wing with root thickness ratio to 18 was also investigated.
Date:
January 1943
Creator:
Harmon, Sidney M.
Partner:
UNT Libraries Government Documents Department