Reference : Unsteady Viscous-Inviscid Coupling Simulations of Separated Laminar Flows Around 2D A...
Scientific congresses and symposiums : Paper published in a book
Engineering, computing & technology : Aerospace & aeronautics engineering
http://hdl.handle.net/2268/183890
Unsteady Viscous-Inviscid Coupling Simulations of Separated Laminar Flows Around 2D Airfoils
English
Rothkegel Ide, José Ignacio mailto [Université de Liège > Département d'aérospatiale et mécanique > Département d'aérospatiale et mécanique >]
Dimitriadis, Grigorios mailto [Université de Liège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale >]
29-Jun-2015
Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015
Paper IFASD-2015011
No
No
International
International Forum on Aeroelasticity and Structural Dynamics
from 28-06-2015 to 02-07-2015
Central Aerohydrodynamics Institute (TsAGI)
Saint Petersburg
Russia
[en] Separated flow ; Boundary layer ; Finite volume ; Panel method ; Double wake ; Vortex blob
[en] An interactive boundary layer model has been developed in 2D in order to solve the unsteady flow around an airfoil. The inviscid problem is solved using a panel method, by the discretization of the airfoil into linear-varying vortex panels. The solution of the boundary layer equations is carried out using a finite volume scheme. Viscous-inviscid coupling is preformed by imposing a permeation velocity on the skin panels of the airfoil and the addition of a free wake at each separation point.
Researchers ; Professionals
http://hdl.handle.net/2268/183890
http://ifasd2015.com

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