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Prediction of aerodynamic characteristics for wings with extensive separations (1981)

Maskew, B. ; Rao, B. M. ; Dvorak, F. A.

In: CASI

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Publication Date: 2019-06-28

Description: The development of a simple yet effective technique for modelling the effects of trailing edge separation is discussed. The model encloses the low energy region with free vortex sheets coupled with a potential flow panel method. The technique includes an interation cycle between viscous and potential flow routines and its development from the two dimensional case to the three dimensional case is discussed. A description of the potential flow panel method, which is based on an internal Dirichlet boundary condition, is included.

Keywords: AERODYNAMICS

Type: AGARD Computation of Viscous-Inviscid Interactions; 15 p

Format: text

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