A Summary of Experimental Data on Wing Characteristics at Transonic Speeds
Aerodynamic Characteristics of Slender Wings in Ground Proximity
Aerodynamics of the Model Airplane. Part 1 - Airfoil Measurements
Report on Proceedings Held by the Wglr Committee on Aerodynamics, on July 10, 1967 in Darmstadt
Some Developments in Aerofoil Theory
Operational V/STOL Transport Aircraft Research Report, 1 Jan. - 31 Jul. 1967
Optimal Payload Trajectory Characteristics for Winged Booster Vehicles
Hypersonic Aerodynamic Characteristics of a Flat-Top Wing Body Combination
Fundamentals in the Theory of a Wing Profile in a Supersonic Flow
Large-Scale Wind-Tunnel Tests of an Airplane Model with Two Propellers and Rotating Cylinder Flaps
Aerodynamic Construction of Transport Airplane Wings for Cruising Flight at High Subsonic Speeds
Hypersonic Aerodynamic Characteristics of Two delta Wing X-15 Airplane Configurations
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
A Design Summary of Stall Characteristics of Straight Wing Aircraft
Airfoil Shape for Flight at Supersonic Speeds
Aerodynamic Characteristics of a Swept Augmentor Wing
Static Aerodynamic Characteristics of a Model with a 17 Percent Thick Supercritical Wing
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
Design of Supercritical Wing Sections with the Aid of Rheoelectrical Analogy
Systems Integration Studies for Supersonic Cruise Aircraft