NASA NTRS · 19820022438
Control software for two dimensional airfoil tests using a self-streamlining flexible walled transonic test section
Abstract
Operation of the Transonic Self-Streamlining Wind Tunnel (TSWT) involved on-line data acquisition with automatic wall adjustment. A tunnel run consisted of streamlining the walls from known starting contours in iterative steps and acquiring model data. Each run performs what is described as a streamlining cycle. The associated software is presented.
Keep this discovery
Explore connections, maps & timelines
Wolf, S. W. D., Goodyer, M. J.. 1982-07-01. Control software for two dimensional airfoil tests using a self-streamlining flexible walled transonic test section. https://ntrs.nasa.gov/citations/19820022438
Cite the original work for its findings. Save a collection to share your selection of sources.