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Aerodynamic Characteristics of Projectile with Exotic Wraparound Wings Configuration
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作者 Fu Zhang Wen-Jun Ruan +2 位作者 Hao Wang Chen-Guang Zhu Meng-Hua Zhang 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2014年第3期30-37,共8页
A projectile with exotic wraparound wings( WAW) configuration is designed to improve the finstabilized projectile shooting quality. Two fin-stabilized projectiles with the same body with and without exotic WAW configu... A projectile with exotic wraparound wings( WAW) configuration is designed to improve the finstabilized projectile shooting quality. Two fin-stabilized projectiles with the same body with and without exotic WAW configuration are simulated numerically by applying the Roe scheme. The shear-stress transport turbulence models and the lower-upper symmetric Gauss-Seidel implicit method are used to solve 3D Reynoldsaveraged Navier—Stokes equations. The differences in aerodynamic coefficients and aerodynamic characteristics of the projectiles when the Mach number varies from 0. 35 to 0. 95 are obtained,and the cause of these differences is analyzed. The calculation results indicate that the lift-to-drag ratio of the projectile significantly increases,the rolling moment decreases,and the position of the pressure center of the projectile shows relatively small changes when the exotic WAW configuration is used. Therefore,this projectile can obviously reduce rolling effect,enlarge range and improve flying stability. 展开更多
关键词 exotic WAW configuration aerodynamic characteristic hybrid structure-unstructured grid overlapping grid
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