Rocket-model Investigation of the Rolling Effectiveness of a Fighter-type Wing-control Configuration at Mach Numbers From
Description: Rolling effectiveness of aerodynamic controls of fighter aircraft with rocket-powered model at transonic speed.
Date: February 25, 1952
Creator: Marley, E. T. & Strass, H. K.
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department