Paper Title:
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.

  Info
Periodical
Edited by
Wenya Tian and Linli Xu
Pages
220-224
DOI
10.4028/www.scientific.net/AMR.186.220
Citation
C. G. Yue, X. L. Chang, Y. H. Zhang, S. J. Yang, "Numerical Calculation of a Missile's Aerodynamic Characteristic", Advanced Materials Research, Vol. 186, pp. 220-224, 2011
Online since
January 2011
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