Geometrically consistent static aeroelastic simulation using isogeometric analysis

In conventional aeroelastic analysis and optimisation methods for wing design, different geometries are used for the different steps in the process. Generally, a parametrised model is used to describe the shape of the geometry for the optimisation process. Subsequently, this model is converted into...

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Veröffentlicht in:	Computer methods in applied mechanics and engineering 2018-10, Vol.340, p.296-319
Hauptverfasser:	Gillebaart, E., De Breuker, R.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aeroelasticity Computation Computer simulation Design optimization Finite element analysis Geometry Isogeometric analysis Meshing Physics Potential flow theory Reissner–Mindlin theory Shell-BEM coupling Wing design
Online-Zugang:	Volltext
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