A new certification approach for bonded primary Fiber Metal Laminate (FML) structures is investigated: using bolts as Disbond Arrest Features (DAF)s to contain the growth of bond line damages so that they can be found and repaired by inspection before becoming critical. By fatigue testing with coupon specimens and model analysis, it has been demonstrated that reducing the Mode I Strain Energy Release Rate (SERR) is the main driver for arrest. The peak stress associated with a disbond front can initiate adherend fatigue cracks during slow growth. The effect of adherend fatigue cracks on the arrest of disbond growth could not be determined and must be investigated in future work. In the process, a novel quasi-analytical disbond growth model h...
Nowadays bonded joints are state of the art in the assembly of composite aircraft structures. Due to...
Fibre metal laminates (FMLs)were developed and refined for their superior crack growth resistance an...
In recent years, carbon fiber-reinforced polymer (CFRP) externally bonded to steel members has been ...
In the development of materials used for constructing aircraft, progress has been made in the produc...
In order for new composite materials like fiber metal laminates (FML) to gain acceptance in the aero...
A parametric finite element model incorporating virtual crack closure technique was developed in ord...
Since fatigue crack can initiate and grow with cyclic stress which is far below than its yield stres...
Adhesively bonded joints have shown great advantages in the aerospace industry when compared with tr...
Fiber metal laminate (FML) is a kind of lightweight material with excellent mechanical properties co...
The excellent durability performance of Glare, a thin fiber metal laminate (FML) material system, is...
© 2017 International Committee on Composite Materials. All rights reserved. Mode I fatigue delaminat...
The use of composite materials in aircraft manufactures increases more and more with the need of lig...
Mechanically fastened joints are susceptible to the presence of multiple-site damage (MSD) cracks in...
The investigation of the present thesis is concerned with the fatigue crack growth behaviour of part...
In this thesis six metal I-beams with a crack repaired by a composite patch been tested in four poin...
Nowadays bonded joints are state of the art in the assembly of composite aircraft structures. Due to...
Fibre metal laminates (FMLs)were developed and refined for their superior crack growth resistance an...
In recent years, carbon fiber-reinforced polymer (CFRP) externally bonded to steel members has been ...
In the development of materials used for constructing aircraft, progress has been made in the produc...
In order for new composite materials like fiber metal laminates (FML) to gain acceptance in the aero...
A parametric finite element model incorporating virtual crack closure technique was developed in ord...
Since fatigue crack can initiate and grow with cyclic stress which is far below than its yield stres...
Adhesively bonded joints have shown great advantages in the aerospace industry when compared with tr...
Fiber metal laminate (FML) is a kind of lightweight material with excellent mechanical properties co...
The excellent durability performance of Glare, a thin fiber metal laminate (FML) material system, is...
© 2017 International Committee on Composite Materials. All rights reserved. Mode I fatigue delaminat...
The use of composite materials in aircraft manufactures increases more and more with the need of lig...
Mechanically fastened joints are susceptible to the presence of multiple-site damage (MSD) cracks in...
The investigation of the present thesis is concerned with the fatigue crack growth behaviour of part...
In this thesis six metal I-beams with a crack repaired by a composite patch been tested in four poin...
Nowadays bonded joints are state of the art in the assembly of composite aircraft structures. Due to...
Fibre metal laminates (FMLs)were developed and refined for their superior crack growth resistance an...
In recent years, carbon fiber-reinforced polymer (CFRP) externally bonded to steel members has been ...