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Application of CFD to high angle of attack missile flowfields
2000
18th Applied Aerodynamics Conference
unpublished
Computational fluid dynamics (CFD) calculations have been performed for a missile body with and without fins. Numerical flow field computations have been made for various Mach numbers and roll angles using an unsteady zonal Navier-Stokes code (ZNSFLOW) and the chimera composite grid discretization technique at supersonic velocity and high angle of attack. Steady-state numerical results have been obtained and compared for cased modeling an ogive-cylinder missile with and without fins. Computed
doi:10.2514/6.2000-4210
fatcat:3lxaucufmngcxjani5zldltg7u