24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-2.2.R.1

A VISCOUS-INVISCID INTERACTION FOR AERODYNAMIC AND AEROELASTIC CALCULATION

W. K. Sekar, C. Weishäupl*, B. Laschka
Institute for Fluid Mechanics, Technische Universität München, Boltzmannstrasse 15, 85748 Garching, Germany; *EADS Military Aircraft, MT242, 81663 Munich, Germany

Keywords: viscous-inviscid interaction, integral boundary layer, TSD equation, Euler equations, state space equation

A viscous - inviscid interaction (VII) to calculate aerodynamic characteristics and its application for flutter calculation of an airfoil or a wing in turbulent flow has been developed at Institute for Fluid Mechanics (FLM) of Technische Universität München (TUM) as an alternative solution of the Navier - Stokes equations.

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