Description: "The author elaborates on the flow phenomena, forces and moments on airfoils in yaw. The existing experiments with straight wings (zero dihedral), wings with dihedral, and wings with sweepback are evaluated within the range of sound angles of attack, explained by calculation and generally enlarged" (p. 1).
Date: August 1939
Creator: Hoerner, Sighard
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department