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AIAA Atmospheric Flight Mechanics Conference
A method to efficiently generate a complete aerodynamic description for projectile flight dynamic modeling is described. At the core of the method is an unsteady, time accurate computational fluid dynamics simulation that is tightly coupled to a rigid projectile flight dynamic simulation. This coupled multidisciplinary technique allows "virtual fly-out" of projectiles on supercomputers, predicts the fight path and all the associated unsteady freeflight aerodynamics of a projectile in andoi:10.2514/6.2009-5715 fatcat:cz7e6pxrxjcddlcwbvxmikjoh4