NASA NTRS · 19680046142
Unit Reynolds number effects on boundary-layer transition at Mach 6.
Abstract
Boundary layer transition measurement on windward side of flat plate in hypersonic wind tunnel, discussing unit Reynolds number effects at Mach 6
Keep this discovery
Explore connections, maps & timelines
Hopkins, E. J., Keener, E. R.. 1968-05-01. Unit Reynolds number effects on boundary-layer transition at Mach 6.. https://ntrs.nasa.gov/citations/19680046142
Cite the original work for its findings. Save a collection to share your selection of sources.