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- W2059053438 abstract "Advances and mo difications to increase the versatility of the SY -TIGER CFD code to compute aerodynamics for a wider variety of flight configurations are presented. Modifications were made to compute the time -dependent aerodynamic performance of spinning missiles. A proce dure for generating a database of aerodynamic stability derivatives for spinning missiles is described. The modified code was applied to two generic spinning missile configurations with excellent comparison to available data. Nomenclature" @default.
- W2059053438 created "2016-06-24" @default.
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- W2059053438 date "2002-06-24" @default.
- W2059053438 modified "2023-09-25" @default.
- W2059053438 title "Computation of Stability Derivatives of Spinning Missiles Using Unstructured Cartesian Meshes" @default.
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- W2059053438 doi "https://doi.org/10.2514/6.2002-2802" @default.
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