A pressure-controllable bump based on the pressure-ridge concept
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DOI: 10.1016/j.ast.2019.02.015
Abstract: Abstract An innovative type of pressure distribution for the hypersonic aircraft forebody (bump) is presented, and this design is based on the newly established known as pressure ridge (PR) flow mechanism. Studies on the low-kinetic-energy… read more here.
Keywords: bump; pressure ridge; controllable bump; pressure controllable ... See more keywords