Description: From Introduction: "In the present paper, under the same lineaeizing assumptions as are made in the derivation in reference 1 but with the explicit consideration and simplification of the form of the wake extending from the rear of the airfoil, the methods of Theodorsen (reference 2) have been extended to obtain the forces on the airfoil not only at a fixed angle of attack but also in arbitrary motion."
Date: June 1, 1947
Creator: Greenberg, J Mayo
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department