Shock-related unsteadiness of axisymmetric spiked bodies in supersonic flow
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DOI: 10.1007/s00348-020-03130-2
Abstract: Abstract Shock-related unsteadiness over axisymmetric spiked body configurations is experimentally investigated at a freestream supersonic Mach number of 2.0 at 0 $$^\circ $$ ∘ angle of attack. Three different forebody configurations mounted with a sharp… read more here.
Keywords: shock; shock related; case; related unsteadiness ... See more keywords