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Unsteady Viscous-Inviscid Coupling Simulations of Separated Laminar Flows Around 2D Airfoils
Rothkegel Ide, José Ignacio; Dimitriadis, Grigorios
2015In Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015
 

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Keywords :
Separated flow; Boundary layer; Finite volume; Panel method; Double wake; Vortex blob
Abstract :
[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.
Disciplines :
Aerospace & aeronautics engineering
Author, co-author :
Rothkegel Ide, José Ignacio ;  Université de Liège > Département d'aérospatiale et mécanique > Département d'aérospatiale et mécanique
Dimitriadis, Grigorios ;  Université de Liège > Département d'aérospatiale et mécanique > Interactions Fluide-Structure - Aérodynamique expérimentale
Language :
English
Title :
Unsteady Viscous-Inviscid Coupling Simulations of Separated Laminar Flows Around 2D Airfoils
Publication date :
29 June 2015
Event name :
International Forum on Aeroelasticity and Structural Dynamics
Event organizer :
Central Aerohydrodynamics Institute (TsAGI)
Event place :
Saint Petersburg, Russia
Event date :
from 28-06-2015 to 02-07-2015
Audience :
International
Main work title :
Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015
Pages :
Paper IFASD-2015011
Additional URL :
Available on ORBi :
since 08 July 2015

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