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Supervised by Ministry of Industry and Information Technology of The People's Republic of China Sponsored by Harbin Institute of Technology Editor-in-chief Yu Zhou ISSNISSN 1005-9113 CNCN 23-1378/T

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Related citation:Fu Zhang,Wen-Jun Ruan,Hao Wang,Chen-Guang Zhu,Meng-Hua Zhang.Aerodynamic Characteristics of Projectile with Exotic Wraparound Wings Configuration[J].Journal of Harbin Institute Of Technology(New Series),2014,21(3):30-37.DOI:10.11916/j.issn.1005-9113.2014.03.005.
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Aerodynamic Characteristics of Projectile with Exotic Wraparound Wings Configuration
Author NameAffiliation
Fu Zhang School of Energy and Power Engineering, Nanjing University of Science and Technology, Nanjing 210094, China 
Wen-Jun Ruan School of Energy and Power Engineering, Nanjing University of Science and Technology, Nanjing 210094, China 
Hao Wang School of Energy and Power Engineering, Nanjing University of Science and Technology, Nanjing 210094, China 
Chen-Guang Zhu School of Energy and Power Engineering, Nanjing University of Science and Technology, Nanjing 210094, China 
Meng-Hua Zhang School of Energy and Power Engineering, Nanjing University of Science and Technology, Nanjing 210094, China 
Abstract:
A projectile with exotic wraparound wings (WAW) configuration is designed to improve the fin-stabilized 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 Reynolds-averaged 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.
Key words:  exotic WAW configuration  aerodynamic characteristic  hybrid structure-unstructured grid  overlapping grid
DOI:10.11916/j.issn.1005-9113.2014.03.005
Clc Number:V11
Fund:

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