NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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
Subject Category
Aerodynamics
Accession Number
81N26068
Funding Number(s)
CONTRACT_GRANT: DAAG29-76-C-0019
CONTRACT_GRANT: N00014-78-C-0128
CONTRACT_GRANT: DAAJ02-75-C-0036
CONTRACT_GRANT: NAS2-8788
Distribution Limits
Public
Copyright
Other
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available