Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7
Description:
From Introduction: "The fundamental integral equation for the pressure distribution on an oscillating thin airfoil moving at subsonic speed has been derived by Possio in reference 1. Collocation procedures have been used by Possio, Frazer, and Skan, and others to obtain lift and moment on an oscillating first plate. An important contribution has been made by Dietze (see reference 2 and 3), who has developed an iterative procedure for numerical solution of Possio's integral equation."
Date:
October 1950
Creator:
Turner, M. J. & Rabinowitz, S.
Partner:
UNT Libraries Government Documents Department