NASA NTRS · 19700000245
Short-duration, transonic flow, variable-porosity test section
Abstract
Short-duration test facility obtains extremely high Reynolds number flows in subsonic, transonic, and supersonic speed ranges, and aids in solving Reynolds number-dependent aerodynamic and thermodynamic problems in design and testing of large, high speed vehicles. The modified blowdown wind tunnel avoids data confusion and aerodynamic noise.
Keep this discovery
Explore connections, maps & timelines
Davis, J. W., Hill, O. E.. 1970-09-01. Short-duration, transonic flow, variable-porosity test section. https://ntrs.nasa.gov/citations/19700000245
Cite the original work for its findings. Save a collection to share your selection of sources.