Numerical Calculation of a Missile's Aerodynamic Characteristic
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.
Wenya Tian and Linli Xu
C. G. Yue et al., "Numerical Calculation of a Missile's Aerodynamic Characteristic", Advanced Materials Research, Vol. 186, pp. 220-224, 2011