Local turbulent skin-friction measurements on a flat plate at mach numbers from 2.5 to 4.5 and reynolds numbers up to 69 x 106
Supersonic wind tunnel tests of turbulent skin friction on flat plate at very high Reynolds number
REYNOLDS NUMBER↗
Engineering topics
Allen, J. M.
Publications and source records attributed to Allen, J. M..
Development of a vapor-pressure-operated high-temperature sensor device final report
Vapor pressure curves of low melting metals for selection of high temperature sensor device
METALLURGY↗
Effects of surface emittance on turbulent skin friction at supersonic and low hypersonic speeds
Surface emittance effect on turbulent skin friction at supersonic and low hypersonic speeds
SUPERSONIC SPEED↗