Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds
Description: From Introduction: "The present paper contains a first-order evaluation of a number of aerodynamic derivatives for a rectangular wing of infinite aspect ratio at finite angles of attack, based upon the linear perturbation theory for rotational flow."
Date: July 1955
Creator: Martin, John C & Malvestuto, Frank S , Jr
Item Type: Refine your search to only Report
Partner: UNT Libraries Government Documents Department