Effects of plan form, airfoil section, and angle of attack on the pressures along the base of blunt-trailing-edge wings at Mach numbers of 1.41, 1.62, and 1.96
Description: No Description Available.
Date: September 16, 1952
Creator: Goin, Kennith L
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department