Title
Methods for numerical simulation of leading-edge vortex flow
Author
Hoeijmakers, H.W.M.
Institution
National Aerospace Laboratory NLR
Date
1984-06-20
Abstract
A review is presented of computational methods to simulate the aerodynamics of configurations with leading-edge vortex flow. The various methods in use at present are discussed in some detail, primarily with a view towards three-dimensional steady flow applications. The strengths and weaknesses of the methods are indicated and results of different methods are compared and discussed. Invited paper presented at Workshop on Vortex Dominated Flows, July 9-10, 1985, NASA Langley Research Center, Hampton, Virginia, USA.
To reference this document use:
http://resolver.tudelft.nl/uuid:23ac090a-fe88-4879-bf9f-48de77cb70fc
Publisher
Nationaal Lucht- en Ruimtevaartlaboratorium
Access restriction
Campus only
Source
NLR MP 85052 U
Part of collection
Aerospace Engineering Reports
Document type
report
Rights
(c) 1984 National Aerospace Laboratory NLR