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Stability of the laminar boundary layer flow encountering a row of roughness elements: Biglobal stability approach and DNS
Institution:1. Département Modèles pour l''Aérodynamique et l''Energétique, ONERA, 2, av. Edouard Belin, BP 4025, 31055 Toulouse Cedex, France;2. Institut für Aerodynamik und Gasdynamik, Universität Stuttgart, Pfaffenwaldring 21, D-70550 Stuttgart, Germany;1. Centre Européen de Recherche et de Formation Avancée en Calcul Scientifique (CERFACS), 42 avenue Gaspard Coriolis, 31057 Toulouse Cedex 01, France;2. ISAE-SUPAERO, 10 avenue Edouard Belin, BP 54032, 31055 Toulouse Cedex 4, France;3. Aix Marseille Univ, CNRS, Centrale Marseille, M2P2 UMR 7340, 13451 Marseille, France;1. ONERA/DMPE, Université de Toulouse, 31055 Toulouse, France;2. ISAE-SUPAERO, Université de Toulouse, 31055 Toulouse, France
Abstract:The stability of the laminar boundary layer developing on a flat plate in the presence of a periodic row of roughness elements is investigated. A Direct Numerical Simulation is performed to compute the steady flow downstream of the roughness elements, which contains a pair of two counter-rotating streamwise vortices per element, which can be considered as a “pre-streaky” structure. The linear stability of this base flow is analyzed by means of the so-called “biglobal” stability approach. Three-dimensional eigenmodes are found, which are shown to be the continuation of the Tollmien–Schlichting waves present in the case of an unperturbed boundary layer. Moreover, a stabilizing effect due to the roughness-induced vortices is found. A Direct Numerical Simulation of the interaction between a two-dimensional Tollmien–Schlichting wave and the roughness array is also performed. The computed perturbation traveling downstream of the roughness elements is shown to be a linear combination of the biglobal eigenmodes.
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