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• W2011183930 abstract "Detached-eddy simulations for the M219 experimental cavity geometry and the 1303 uninhabited combat airvehicle cavity geometry are presented. First, results from three computations are presented with the aim of studyingthe effect of imposing synthetic velocity fluctuations at the inflow boundary. Both methods employed (synthetic-eddymethod and fluctuations from a precursor large-eddy simulation) increased the high-frequency content in theboundary layer upstream of the cavity. Averaged profiles showed little change in the streamwise velocity; however,the profiles of normal velocity were noticeably different. The influence of the upstream boundary layer on the cavityflowfield means that the full aircraft geometry needed to be modeled. Consequently, advanced multiblock topologieshad to be used to properly represent the planform of the uninhabited combat air vehicle and all the details of thecavity, including doors and hinges, while sliding meshes were needed to insert the store into the uninhabited combatair vehicle configuration. Results with an empty cavity were encouraging for such complex configurations.Visualizations using the Q criteria revealed the added turbulent content due to the door leading edges and the doorhinges. The addition of a store in between the doors had little effect close to the front wall. However, averagedflowfields showed that the proximity of the shear layer to the apex of the store deflected it downward into the cavityand restricted its growth. Outside the cavity, shedding was observed from the sting and force balance." @default.
• W2011183930 created "2016-06-24" @default.
• W2011183930 creator A5023557804 @default.
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• W2011183930 date "2010-09-01" @default.
• W2011183930 modified "2023-10-16" @default.
• W2011183930 title "Computational Fluid Dynamics Analyses of Flow over Weapons-Bay Geometries" @default.
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• W2011183930 doi "https://doi.org/10.2514/1.c000218" @default.
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