TsAGI Science Journal
Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
MODELING OF THE LAMINAR−TURBULENT TRANSITION ON A SWEPT AND STRAIGHT WINGS WITH THE USE OF NUMERICAL SOLUTIONS OF THE NAVIER−STOKES EQUATIONS
Volumen 46,
Edición 4, 2015,
pp. 309-322
DOI: 10.1615/TsAGISciJ.2015015524
SINOPSIS
Application of the state-of-the-art turbulence model based on the transport equation for the intermittency in calculating the position of laminar-turbulent transition on the swept wing surface is investigated. The theoretical characteristics of the laminar-turbulent transition for straight and swept wings with LV6 airfoil are compared. The comparative analysis of the results of calculation of boundary layer characteristics and the data of tests in a T-124 low-level turbulence wind tunnel of TsAGI is performed.
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