E. Dikbaş, C. Schnepf, M. Tormalm, Michael Anderson, S. Shaw, J. Despirito, G. Loupy, G. Barakos, K. Boychev, C. Toomer, O. Baran
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引用次数: 1
Abstract
A research program has been underway for four years to study vortex interaction aerodynamics that are relevant to military air vehicle performance. The program has been conducted under the auspices of the NATO Science and Technology Organization (STO), Applied Vehicle Technology (AVT) panel by a Task Group with the identification of AVT-316. The Missile Facet of this group has concentrated their work on the vortical flow field around a generic missile airframe and its prediction via computational methods. This paper focuses on mesh-related effects and RANS simulations. Simulated vortex characteristics
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