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- W2370711515 abstract "In order to study the aerodynamic interference effect of single and multiple blunt body for rectangular section,reverse right angle section,reverse inter convex arc section and reverse outer convex arc section,based on the finite volume method and the SIMPLE algorithm,the uniform viscous and incompressible fluid around blunt bodies when Reynolds number was in the subcritical area was simulated by computation fluid dynamics(CFD) technology.The aerodynamic coefficients under different conditions such as different wind angles of attack,different chamfer dimensions and different cylinder spacings,etc.were calculated and the change of aerodynamic coefficient was analyzed.The results show that(1) the drag and lift as well as torque coefficients of each section of single blunt body decrease in accordance with the sequence of rectangular section,reverse right angle section,reverse concave arc section and reverse convex arc section as a whole during different wind angles of attack,while the drag and lift as well as torque coefficients of reverse right angle section,reverse concave arc section and reverse convex arc section decrease successively when chamfer dimension increases;(2) the downstream blunt body produced bigger change than upstream blunt body both in variation trend and value due to aerodynamic interference effect." @default.
- W2370711515 created "2016-06-24" @default.
- W2370711515 creator A5066602508 @default.
- W2370711515 date "2012-01-01" @default.
- W2370711515 modified "2023-09-26" @default.
- W2370711515 title "Numerical Simulation of Aerodynamic Interference Effect of Three-component Force Coefficient on Serial Blunt Body" @default.
- W2370711515 hasPublicationYear "2012" @default.
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