Use of a scale model in the design of modifications to the NASA Glenn Icing Research Tunnel

Subsonic aerodynamic assessment of vortex flow management devices on a high-speed civil transport configuration

Bryan A. Campbell

A universal three-dimensional wall pressure correction method for closed rectangular subsonic wind tunnel test sections (displacement, downwash, streamline curvature)

Gerhard Schulz

Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel

Gregory S. Manuel

Design of a new contraction for the ARL low speed wind tunnel (U)

J. H. Watmuff

Design & fabrication of a traversing mechanism and glide slope mechanism for the UTIAS wind tunnel

Hussein Amr Sabbour

The Langley 14- by 22-foot subsonic tunnel: description, flow characteristics, and guide for users

Garl L. Gentry