Stephen W. D. Wolf

• Adaptive wall technology for minimization of wall interferences in transonic wind tunnels
• Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
• Highlights of experience with a flexible walled test section in the NASA Langley 0.3 meter transonic cryogenic tunnel
• NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6
• Predictive wall adjustment strategy for two-dimensional flexible walled adaptive wind tunnel
• Supersonic wind tunnel nozzles
• Wall adjustment strategy software for use with the NASA Langley 0.3-meter transonic cryogenic tunnel adaptive wall test section