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- W3205118022 abstract "The purpose of this paper is to investigate numerically the flow around a projectile with an axis parallel to the free flow. The flow separation in the trailing edge and the shape of the resultant wake has been studied at Reynolds number 10,000 (based on D). By changing the fineness ratio (L/D) of the cylinder, its effects on separation and the drag coefficient has been obtained. The effect of presence or absence of conical head has been investigated. The applied turbulence model is kωSST. By studying the results, it can be found that for a high fineness ratio with growth of the boundary layer, the flow reattaches while at low fineness ratios the flow still separated and this is effective on the shape of the resultant wake and the drag coefficient. Using a conic head will delay the separation and reduce the drag." @default.
- W3205118022 created "2021-10-25" @default.
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- W3205118022 date "2018-03-11" @default.
- W3205118022 modified "2023-09-23" @default.
- W3205118022 title "Numerical Solution of Axial Flow around a Projectile" @default.
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