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
Application of a Supercritical Wing to an Executive-Type Jet Transport Model
General Survey of Computer-Methods Used for Aerodynamic Design in the Federal Republic of Germany
Effect of Wing Bend on the Experimental Force and Moment Characteristics of an Oblique Wing
Theoretical and Experimental Investigation of Noise Shielding for Jet Engines
Effect of Flap Deflection on the Lift Coefficient of Wings Operating in a Biplane Configuration