We describe the evolution of a Navier-Stokes code developed in the Israel Aircraft Industries and its application to complex turbulent high-Reynolds flows. The paper focuses on the following issues: 1) implementation and validation of the Spalart-Allmaras turbulence model, 2) parallelization of the computational framework, and 3) application to the design of the wing-body fairing of a generic business jet.The improved capability of the code allowed its use for large-scale flow simulations on a daily basis
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Seror et al. (2005) studied this question.
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