Title: Computations with k-g Model for Complex Configurations at High-Incidence
Abstract:The two-equation k-g turbulence model, a derivation of the k-w model, with its advantages such as no use of normal-to-wall distance, simple source terms, and straightforward boundary conditions, can b...The two-equation k-g turbulence model, a derivation of the k-w model, with its advantages such as no use of normal-to-wall distance, simple source terms, and straightforward boundary conditions, can be easily applied in complex computational fluid dynamics applications. Transonic flows around the ONERA M6 wing and the NASA TN D-712 wing-fuselage model at angles of attack of 12.5 and 26.2 deg are first used to validate the codes. Then the transonic flows around an F-22-like complete aircraft configuration are numerically simulated at angles of attack from 0 to 48 degRead More
Publication Year: 2005
Publication Date: 2005-03-01
Language: en
Type: article
Indexed In: ['crossref']
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Cited By Count: 11
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