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

The real-time wall interference correction system of the NASA Ames 12-foot pressure wind tunnel

Norbert Ulbrich

The 13-inch magnetic suspension and balance system wind tunnel

William G. Johnson

Study of the unsteady flow features on a stalled wing

S. Yon

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

Bryan A. Campbell

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

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

Victor A. Canacci