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:
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Partner:
UNT Libraries Government Documents Department