Analysis of the Mechanical Response of Impact Loaded Composite Sandwich Structures with Focus on Foam Core Shear Failure.

Annotation

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Block, Tim Berend
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Berlin : Logos Verlag Berlin, 2014.
Colección:Science-Report Aus Dem Faserinstitut Bremen Ser.
Temas:
Materials > Testing.
Matériaux > Essais.
Materials > Testing
Acceso en línea:Texto completo

MARC

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049 |a UAMI 
100 1 |a Block, Tim Berend. 
245 1 0 |a Analysis of the Mechanical Response of Impact Loaded Composite Sandwich Structures with Focus on Foam Core Shear Failure. 
260 |a Berlin :  |b Logos Verlag Berlin,  |c 2014. 
300 |a 1 online resource (238 pages). 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Science-Report Aus Dem Faserinstitut Bremen Ser. ;  |v v. 9 
588 0 |a Print version record. 
505 0 |a Intro; 1 Introduction; 1.1 Motivation; 1.2 Objective; 1.3 Thesis structure; 2 State of the art of composite sandwich technology; 2.1 Application of composite sandwich structures; 2.2 Materials and manufacturing; 2.3 Fundamentals of composite sandwich theory; 2.3.1 Localized loads on sandwich beams; 2.3.2 Failure modes of sandwich beams; 2.3.3 Failure mode maps; 2.4 Chapter summary; 3 Impact response of composite sandwich structures; 3.1 Definitions; 3.2 Literature review; 3.3 Classification of the structural impact response; 3.4 Contact behavior and indentation of sandwich panels. 
505 8 |a 3.5 Sandwich failure modes during impact3.6 Chapter summary; 4 Experimental investigation of the impact response; 4.1 Test matrix and setup; 4.2 Test results at room temperature; 4.3 Test results at low temperatures; 4.4 Classification of damage types; 4.5 Comparison with analytical model; 4.6 Chapter summary; 5 Numerical simulation of impact on CFRP foam core sandwich structures; 5.1 General aspects; 5.1.1 Basic equations and explicit time integration scheme; 5.1.2 Modeling approach; 5.1.3 Thermal effects; 5.2 Modeling of the CFRP face sheets; 5.2.1 Mechanical behavior of CFRP. 
505 8 |a 5.2.2 Material properties and strain rate sensitivity5.2.3 Experiments; 5.2.4 Simulation with one element across the thickness; 5.2.5 Simulation with one element per ply; 5.3 Modeling of the foam core; 5.3.1 Mechanical behavior and applied material model; 5.3.2 Experiments; 5.4 Modeling of the sandwich structure; 5.4.1 Interface crack growth; 5.4.2 Static indentation of sandwich panels; 5.4.3 Thermal loads and strain rates; 5.5 Simulation of low velocity impact; 5.5.1 Impact response; 5.5.2 Damage size and impact failure mode; 5.6 Chapter summary; 6 Sandwich failure mode parameters. 
505 8 |a 6.1 Approach6.2 Thermal loads; 6.3 Boundary conditions; 6.4 Impactor geometry and velocity; 6.5 Material properties of face sheet and core; 6.6 Chapter summary; 7 Concluding remarks; 7.1 Summary of performed work; 7.2 Limitations and implications; 7.3 Future work. 
520 8 |a Annotation  |b Sandwich structures are an economically and structurally efficient way of designing large integral composite parts. In the aerospace industry pre-impregnated face sheets and honeycomb core structures can be considered as industry standard while e.g. naval structures and wind turbine blades typically use vacuum infusion technology with polymer foam cores. Application of the less costly infusion technology in the aeronautical industry requires a thorough understanding of the damage tolerance including low velocity impact as a frequent source of damaging events. At low impact energies damage in composite foam core sandwich structures is limited to core crushing and local face sheet delaminations. Higher impact energies may initiate the competing failure modes face sheet rupture and core shear failure depending on impact, geometric and material parameters. Face sheet rupture leads to severe local damage with typically good visibility, while core shear failure leads to cracks and rear face sheet debonding of the foam core with less visibility. This work investigates the low velocity impact response of sandwich structures with carbon fiber reinforced plastic (CFRP) face sheets and a polymeric foam core using experiments at room temperature and at -55 Grad Celsius. An analytically derived failure mode map is presented as a simple tool for design guidelines while the explicit finite element method is applied for a more detailed description of the sandwich impact process. Both models are used to analyze the impact response and describe relevant sensitivity parameters of sandwich structures. 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Materials  |x Testing. 
650 6 |a Matériaux  |x Essais. 
650 7 |a Materials  |x Testing  |2 fast 
776 0 8 |i Print version:  |a Block, Tim Berend.  |t Analysis of the Mechanical Response of Impact Loaded Composite Sandwich Structures with Focus on Foam Core Shear Failure.  |d Berlin : Logos Verlag Berlin, ©2014  |z 9783832538538 
830 0 |a Science-Report Aus Dem Faserinstitut Bremen Ser. 
856 4 0 |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=5231220  |z Texto completo 
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938 |a YBP Library Services  |b YANK  |n 15138965 
994 |a 92  |b IZTAP 

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