Experimental Study of Flow About a Stalled Two-Dimensional Airfoil
Mechanization and Utilization of Variable Camber in Fighter and Attack Airplanes
Analysis of the Influence of Aircraft Design Parameters on Air-to-Air Combat Capability
Aerodynamic Characteristics of a Swept Augmentor Wing
Static Aerodynamic Characteristics of a Model with a 17 Percent Thick Supercritical Wing
A Design Summary of Stall Characteristics of Straight Wing Aircraft
Airfoil Shape for Flight at Supersonic Speeds
Hypersonic Cruise Vehicle Wing Structure Evaluation
A Contribution to the Theory of Multiweb Wing Structures
Aircraft Design Studies - Counter Insurgency Aircraft with Suction Boundary Layer Control
Effect of Wing Tip Configuration on the Strength and Position of a Rolled-Up Vortex