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BALLISTIC AND AIRDYNAMICS

Study of Aerodynamic Characteristics of Wing-body Configuration with Very Low Aspect Ratio

  • DING Yu ,
  • LI Bin ,
  • LIU Xianming ,
  • WANG Xuezhan
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2009-08-26

  Online published: 2025-05-28

Abstract

In order to reduce the lateral force by controlling the asymmetric vortexes, the effect of strakes on the forebody was investigated. The flow over very low aspect ration wing-body configuration with/without forebody strakes was simulated using finite volume method. The free Mach number was 0.8, and the Reynolds number was 2.36×105. The results indicate that the side force is reduced by forebody strakes; the drag force and the normal force are insensitive to the forebody strakes.

Cite this article

DING Yu , LI Bin , LIU Xianming , WANG Xuezhan . Study of Aerodynamic Characteristics of Wing-body Configuration with Very Low Aspect Ratio[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(3) : 135 -137,144 . DOI: 10.15892/j.cnki.djzdxb.2010.03.038

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References

[1]
Coe P L,Chambers J R,Letko W.Asymmetric lateral directional characteristics of pointed bodies of revolution at high angles of attack,NASAT N D-7095[R].1972.
[2]
Dunne A L,Black S,Schmidt G S,et al.VLA missile development and high angle of attack behavior,NEAE, CA[R].1988.
[3]
Ericssion L E, Beyers M E. Fluid mechanics considerations for successful design of forebody flow control, AIAA 2000-2320[R]. 2000.
[4]
顾蕴松, 明晓. .大迎角非对称流动的非定常弱扰动控制[J]. 航空学报, 2003,24(2):102-106.
[5]
Levy Y, Hesselink L, Degani D. Systematic study of the correlation between geometrical disturbances and flow asymmetries, AIAA 95-21474[R]. 1995.
[6]
Kistan P, Stephen G G. Effect of forebody strakes on a CFD-created asymmetric flowfield, AIAA 2006 3843[R]. 2006.
[7]
Yuan C C, Howard R M. The effects of forebody strakes on a missile[J]. Journal of Spacecraft and Rockets, 1991 (4): 411- 417.
[8]
Westmoreland S, Gebert G. Strake effectiveness for controlling out-of-plane loading on missile configuration, AIAA 2000-0386[R]. 2000.
[9]
Logan W V, Davis R L, Sarigul-Klijn N. Forebody strake effects on rocket aerodynamic characteristics at high angles of attack[J]. Journal of spacecraft and rockets, 2008, 45 (4): 691- 697.
[10]
Menter F R. Two equation eddy viscosity turbulence models for engineering applications[J]. AIAA Journal, 1994, 32 (8): 1598- 1605.
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