A Wind-tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 degree Sweptback Wing at Transonic Speeds
Description: Effects of deflected inboard ailerons on wing loads of 45-deg swept-back wing at transonic speeds.
Date: July 21, 1958
Creator: Heath, A. R., Jr. & Igoe, A. W.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department