Analysis of aerodynamic characteristics of a modular assembled missile with canard rudder and arc tail

Chen, Han; Li, Kewei; Wang, Chao; Xia, Fei; Li, Bin; Wang, Shikun; Deng, Hongbin; Zhai, R. Grace; Xia, Zongze

doi:10.1109/icmic.2017.8321598

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2019

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“…Flow about axi-symmetric canard controlled missile with wrap around tail fin is simulated using ANSYS FLUENT. Wrap around fins configurations is a major field of research [5]. The simulations are performed for several angles of attack as well as several control deflections.…”

Section: Introductionmentioning

confidence: 99%

Numerical and Experimental Determination of Canard Controlled Missile Aerodynamic Coefficients in Subsonic Regime

2019

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This paper discusses the computational and experimental approach to the determination of aerodynamic coefficients of canard controlled missile with wrap around tail fin. The paper presents results of subsonic flow at Mach 0.4. Angle of attack of the missile is varied from −10 to +10 degrees with an increment of 2 degrees. Canard deflection in the pitch plane is also varied at 0, 10, and 15 degrees. The results of the simulation are compared with the experimental data obtained by the wind tunnel measurements. Measured results confirm applicability of Spalart Allmaras turbulence model with adapted computational mesh to the determination of aerodynamic coefficients for canard controlled missiles.

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Section: Introductionmentioning

confidence: 99%