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The unsteady aerodynamic forces are computed using computational fluid dynamics (CFD) methods assuming aerodynamic symmetry.
These indexes are computed using real μ-analysis.
The structure responses are computed using dynamic finite element analysis.
The optimal controls are computed using Dynamic Programming (DP).
Trajectories are computed using the global forecast data3, GFS model run from October 12th, 2015.
Questions are asked in the form of a piece of code whose answers are computed using the pseudonymized data.
The electric and magnetic fields for the fundamental core-mode HE11 are computed using the finite-element-method.
The limit states are computed using deterministic FE analyses.
The integrals involving plastic region are computed using internal cells.
Results are computed using numerical integration and finite element techniques.
Additionally, all these flows are computed using a CFD methodology.
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