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A quasi-steady representation is used to model the aerodynamic force.
Krumhaar's modified supersonic piston theory, which considers the radius effect, is adopted to model the aerodynamic loading.
The unsteady representation based on the Duhamel formulation is used to model the aerodynamic lift and moment.
An NACA0015 airfoil is used for the baseline model; the aerodynamic characteristics of the base model are compared with that of the optimal solutions.
The hysteric damping model is used to describe the viscoelastic property of the mid-layer material and the first piston theory to model the aerodynamic forces.
Aeroacoustic formulations in time domain are frequently used to model the aerodynamic sound of airfoils, the time data being more accessible.
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JSBSim models the aerodynamic forces and moments by the classic coefficient buildup method.
An analytical formulation for modelling the aerodynamic loads within the finite element is assumed in conformity with classical flutter analysis.
We thus conclude that the ME technique is both necessary and sufficient for modeling the aerodynamic coefficients for surrogate-based mission analysis.
For modelling the aerodynamic forces of the wing steady linear and non-linear models as well as an unsteady model were used.
Furthermore, modeling the aerodynamic forces that act on low altitude satellites is a formidable task, especially for objects of a complex shape and unknown attitude evolution.
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Justyna Jupowicz-Kozak
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