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Dive into the research topics where Axel Fink is active.

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Featured researches published by Axel Fink.


Composite Joints and Connections#R##N#Principles, Modelling and Testing | 2011

Reinforcement of composite bolted joints by means of local metal hybridization

Axel Fink; P.P. Camanho

Abstract: The use of a local hybridization with metal represents a suitable and technologically feasible means of increasing the mechanical efficiency of highly loaded composite bolted joints. This technology allows significant improvement of the overall structural efficiency of real composite structures. Contrary to conventional reinforcement concepts with metal, the local laminate hybridization entails the implementation of thin high-strength metal foils within the laminate by means of either ply substitution or ply addition techniques. This chapter addresses some fundamental aspects of the mechanical behaviour of hybrid joints in terms of its reinforcement effect, the damage behaviour and the impact of geometric and material-related parameters.


Composite Structures | 2008

CFRP/titanium hybrid material for improving composite bolted joints

Boris Kolesnikov; Lars Herbeck; Axel Fink


Composites Science and Technology | 2010

Hybrid CFRP/titanium bolted joints: Performance assessment and application to a spacecraft payload adaptor

Axel Fink; P.P. Camanho; J.M. Andrés; E. Pfeiffer; A. Obst


Composites Part A-applied Science and Manufacturing | 2009

Hybrid titanium-CFRP laminates for high-performance bolted joints

P.P. Camanho; Axel Fink; A. Obst; S. Pimenta


Archive | 2003

Hybrid Titanium composite Material improving Composite Structure Coupling

Axel Fink; Boris Kolesnikov; H. Wilmes


Archive | 2002

New Design Concepts for an CFRP Fuselage

H. Wilmes; Boris Kolesnikov; Axel Fink; C. Kindervater


Archive | 2008

Faserverbundstruktur und Herstellungsverfahren dafür

Axel Fink; Christian Hühne; Markus Kleineberg; Boris Kolesnikov; Arne Stahl


Archive | 2009

Composite material for optimized high-strength coupling of stringer to aerofoil of aircraft, has intermediate layer exhibiting small rigidity than adjacent non-continuous fiber composite layer and reinforcement material layer

Stephan Erwig; Axel Fink; Lars Herbeck; Boris Kolesnikov


Archive | 2008

Semimonocoque-structured panel for use in e.g. airbus A-320, has stringer with hat profile exhibiting surface curved in direction of axis and transverse direction, where width of profile in transverse direction is set between frames

Axel Fink; Michael Hanke; Lars Herbeck; Christian Hühne; Markus Kleineberg; Boris Kolesnikov; Thomas Dipl.-Ing. Kruse


Archive | 2008

Fibrous composite structure comprises two plate-like construction units, where overlapping range and contact surface are provided in construction units

Axel Fink; Christian Hühne; Markus Kleineberg; Boris Kolesnikov; Arne Stahl

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Lars Herbeck

German Aerospace Center

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Heiko Assing

German Aerospace Center

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H. Wilmes

German Aerospace Center

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