EUCASS book series - Advances in AeroSpace Sciences

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

Published online: 14 June 2013

DOI: 10.1051/eucass/201305081

N. V. Semionov

A. D. Kosinov

Yu. G. Yermolaev

R. I. Kazantsev

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