Journal article
3D high lift flow computations using HiFUN
Abstract
A summary of the results obtained using the flow solver HiFUN for the 3D High lift NASA Trapezoidal wing are presented. Hybrid unstructured grids have been used for the computations. Grid converged solution obtained for the clean wing and the wing with support brackets, are compared with experimental data. The ability of the solver to predict critical design parameters associated with the high lift flow, such as αmax and CLmax$$C_{L_{max}}$$ …
Authors
Gopalakrishna N; Ravindra K; Shende NV; Balakrishnan N
Journal
International Journal of Advances in Engineering Sciences and Applied Mathematics, Vol. 6, No. 3-4, pp. 222–241
Publisher
Springer Nature
Publication Date
12 2014
DOI
10.1007/s12572-015-0124-3
ISSN
0975-0770