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Experimental study of stability and transition of supersonic boundary layer on swept wing at mach number 2-4

N. V. Semionov, A. D. Kosinov, Yu. G. Yermolaev and R. I. Kazantsev

EUCASS Proceedings Series – Advances in AeroSpace Sciences, 5 (2013) 81-92

DOI: https://doi.org/10.1051/eucass/201305081

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