Numerical Calculation of a Missile's Aerodynamic Characteristic

Chun Guo Yue; Xin Long Chang; You Hong Zhang; Shu Jun Yang

doi:10.4028/www.scientific.net/AMR.186.220

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HomeAdvanced Materials ResearchAdvanced Materials Research Vol. 186Numerical Calculation of a Missile's Aerodynamic...

Numerical Calculation of a Missile's Aerodynamic Characteristic

Abstract:

In virtue of Fluent of CFD software, numerical computations of aerodynamics of an air-to-air missile in different mach numbers and different attack angles were carried though. The movement trends of lift coefficient, drag coefficient and pitching moment coefficient with variety of mach numbers and attack angles were gained, meanwhile, distributing trends of pressure, temperature and weather velocity were also obtained. The results indicated that the basis and references could be offered by numerical computation results for shape design of missile and definite preponderances were showed than traditionary numerical computation methods.

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Periodical:

Advanced Materials Research (Volume 186)

Pages:

220-224

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.186.220

Citation:

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Online since:

January 2011

Authors:

Chun Guo Yue, Xin Long Chang, You Hong Zhang, Shu Jun Yang

Keywords:

Attack Angle, Drag Coefficient, Fluent, Lift Coefficient, Pitching Moment Coefficient

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