Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers
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DOI: 10.1063/5.0022015
Abstract: The experimental analysis of base pressure in a high-speed compressible flow is carried out. The flow is made to expand abruptly from the nozzle into an enlarged duct at fifteen sonic and supersonic Mach numbers.… read more here.
Keywords: base pressure; supersonic mach; sonic supersonic; mach numbers ... See more keywords