21-RANS-based models predictions
Laminar-turbulent transition prediction for hypersonic vehicle with RANS-based models. Laurent MUSCAT1, Marina OLAZABAL1 1CEA CESTA, 15 Avenue des Sablières CS60001, 33116 Le Barp CEDEX, France. E-mail: laurent.muscat@cea.fr Keywords: RANS-based transition method, crossflow, hypersonic experimental vehicle. Abstract The prediction of the boundary layer transition has a significant impact on the design of hypersonic aircraft. […]

