Computational Aerodynamics of the C-130 in Airdrop Configurations

Author:

Serrano Matthieu1,Leigh Elliot2,Johnson William2,Forsythe James2,Morton Scott2

Affiliation:

1. Ecole Polytechnique

2. U.S. Air Force Academy

Publisher

American Institute of Aeronautics and Astronautics

Reference19 articles.

1. Spalart, P.R. and Allmaras, S.R., 1994,"A One-Equation Turbulence Model for Aerodynamic Flows,'' La Recherche Aemspatiale 1,pp. 5-21. Spalart, P. R. , Jou W-H. , Strelets M. , and Allmaras, S. R. "Comments on the Feasibility of LES for Wings, and on a Hybrid RANS/LES Approach," Advances in DNS/LES, 1st AFOSR Int. Conf.onDNS/LES, Aug4-8,1997, Greyden Press, ColumbusOh.

2. Detached-eddy simulation of an airfoil at high angle of attack

3. Travin, A., Shur, M., Strelets, M., and Spalart, P.R., 2000, "Detached-EddySimulationPastaCircularCylinder,"Int. J. Flow, Ihrbulence and Combwtion, 63(1-4),pp. 293-313.

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