Relaminarization of a turbulent boundary layer with a mach number M∞=4
M. A. Goldfeld, R. V. Nestoulia, A. N. Shiplyuk
Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk 630090
Abstract
Results of experimental studies are
presented on relaminarization of a
supersonic turbulent boundary layer
behind an expansion fan for a free-
stream Mach number M∞=4
within a range of Reynolds numbers
Re1 = 8
