NASA NTRS · 19680058556
A perforated-wall nozzle for variable Mach number testing.
Abstract
Perforated wall nozzle providing variable Mach number supersonic flow for external stream simulation in rocket propulsion tests
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Hendershot, K. C., Martin, J. F., Sheeran, W. J.. 1968-09-01. A perforated-wall nozzle for variable Mach number testing.. https://ntrs.nasa.gov/citations/19680058556
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