New hail impact simulation models on composite laminated wing leading edge

Purpose The risk of hail-impact occurrence that can decrease local strength property must be taken into account in the design of primary airframe structures in aviation, energy and space industries. Because of the high-speed of hail impact in operation, it can affect the load carrying capacity. Test...

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Veröffentlicht in:	Aircraft engineering 2019-03, Vol.91 (3), p.457-465
Hauptverfasser:	Kustron, Kamila, Horak, Vaclav, Doubrava, Radek, Goraj, Zdobyslaw Jan
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft Aircraft components Aircraft design Aircraft structures Airframes Aviation Bearing strength Carbon Carbon-epoxy composites Civil aviation Composite materials Composite structures Computational fluid dynamics Computer simulation Finite element analysis Finite element method Flat panels Fluid flow Hail High speed Impact analysis Impact tests Laboratories Load carrying capacity Noise control Polymer matrix composites Projectiles Shells (structural forms) Simulation Smooth particle hydrodynamics Structural design Velocity
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