Stability and Controllability of Supersonic Aircraft
Analytical Investigation of Variable Camber Concepts
Stability and Controllability of Supersonic Aircraft
Results of 1967 Research on Conceptual Flutter Analyses
Vortex Wake Turbulence. Flight Tests Conducted During 1970
Fabrication and Testing of the Composite Materials Aircraft Wing Section
Research Study of Airframe Cost Factors -Supersonic Transport Phase
A Dynamic Simulation Study of the Sweptwing Transport Aircraft in Severe Turbulence
Facilities and Techniques for Aerodynamic Testing at Transonic Speeds and High Reynolds Number