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A set of airfoil agnostic parameters for this model are obtained that permit accurate two-dimensional transonic aeroelastic simulations.
Parameters in this model are obtained from experimental binary and ternary data reported previously.
The sliced contours of the model are obtained based on a given layer thickness at first.
The driving inputs for this simulation model are obtained from a powertrain model.
The normal forms of differential algebraic control system model are obtained by MIMO feedback linearization technique.
Simplified solutions of both the standard model and Maxwell model are obtained under certain conditions.
The equations of motion for a simpler model are obtained by modal expansion.
The materials parameters for the model are obtained from a set of load relaxation experiments.
The steady-state periodic solutions of this model are obtained analytically.
Numerical solutions for a plane strain unit cell model are obtained numerically.
We show that the Tullock contest model and the first-prize sealed-bid auction model are obtained as special cases.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com