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Structural Analysis and Performance-Based Validation of a Composite Wing Spar
CBR-Beta Design Procedure for Aggregate-Surfaced Airfield Pavements
Control of Circulation around a Circular Cylinder
Aerodynamic Design and Analysis of the AST-200 Supersonic Transport Configuration Concept
On the Zero-Lift-Wave-Drag of Wings Depending on the Thickness-Distribution and Planform
Additional Studies of the Effects of Deformation on the Aerodynamic Characteristics of a Sailwing
Hydroaerodynamic Characteristics of Delta Low Aspect-Ratio Configuration Wing Near Screen
Conditions for the Construction of Gliders with a Lift-Drag Ratio of 100
Research Study on Panel Flutter Aerodynamics Final Report, Apr. 5, 1965 - Nov. 4, 1966
Preliminary Sizing and Performance Evaluation of Supersonic Cruise Aircraft