Prediction of aerodynamic characteristics for wings with extensive separationsThe 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.
Document ID
19810017532
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Maskew, B. (Analytical Methods, Inc. Bellevue, WA, United States)
Rao, B. M. (Analytical Methods, Inc. Bellevue, WA, United States)
Dvorak, F. A. (Analytical Methods, Inc. Bellevue, WA, United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1981
Publication Information
Publication: AGARD Computation of Viscous-Inviscid Interactions