Stanley R. Cole

• Divergence study of a high-aspect ratio, forward-swept wing
• Dynamic response of a hammerhead launch vehicle wind-tunnel model
• Effects of spoiler surfaces on the aeroelastic behavior of a low-spect-ratio rectangular wing
• Flutter of a low-aspect-ratio rectangular wing
• Some buffet response characteristics of a twin-vertical-tail configuration
• The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel