NASA NTRS · 20040015218
Tunnel Correction for Compressible Subsonic Flow
Abstract
This report presents a treatment of the effects of the tunnel walls on the flow velocity and direction in a compressible medium at subsonic speed by an approximate method. Calculations are given for the rotationally symmetric and two- dimensionl problems of the flow past bodies, as well for the downwash effect in the tunnel with circular cross section.
Keep this discovery
Explore connections, maps & timelines
Baranoff, A. V.. 1947-07-01. Tunnel Correction for Compressible Subsonic Flow. https://ntrs.nasa.gov/citations/20040015218
Cite the original work for its findings. Save a collection to share your selection of sources.