Experimental study of unsteadiness in supersonic shock-wave/turbulent boundary-layer interactions with separation

Publisher: Cambridge University Press

E-ISSN: 2059-6464|114|1155|299-308

ISSN: 0001-9240

Source: The Aeronautical Journal, Vol.114, Iss.1155, 2010-05, pp. : 299-308

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Abstract