Journal of Aircraft · 1999 · 41 citations · 6 references
EngineeringAerospace EngineeringComputational EngineeringComputational Fluid DynamicsComputational MechanicsFluid DynamicsComputational AerodynamicsMultibody DynamicsWind-tunnel TestingSix-degree-of-freedom SimulationWind Tunnel Simulation
The Beggar code uses blocked and overset grid techniques and combines the grid assembly, e ow solution, and six-degree-of-freedom trajectory calculation processes into a single code with reduced user input. Its capabilities to handle moving body problems are demonstrated through a series of store separation trajectory calculations. Single-storeseparationtrajectorycalculationsattransonicMachnumbersarecomparedwithpreviouslypublished wind-tunnel data. Supersonicstoreseparation predictionsare compared with previously unpublished wind-tunnel data. The generality and ease of use are further illustrated by a three-store ripple release simulation.
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