Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap
Description: From Introduction: "The present report gives results at a Mach number of 4.04 of the part of the program concerned with flap controls at Mach numbers from 1.62 to 6.9."
Date: May 29, 1953
Creator: Dunning, Robert W & Ulmann, Edward F
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department