When unidirectional fiber reinforced polymer composites are loaded in tension-tension fatigue multiple fiber breaks occur in random positions during the first cycle. Assuming that fibers do not experience fatigue, the further damage evolution with increasing number of cycles is in form of debonds growing along the fiber/matrix interface. Fracture mechanics analysis is performed to compare this mechanism with an alternative one where debonds initiate from transverse matrix cracks.Godkänd; 2009; Bibliografisk uppgift: CD-ROM; 20091103 (ysko
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
The aim of this paper is to analyse fibre/matrix debond crack growth during high stress cyclic tens...
When unidirectional fiber reinforced polymer composites are loaded in tension-tension fatigue multip...
When unidirectional fiber reinforced polymer composites are loaded in tension-tension fatigue multip...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) c...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
When a unidirectional (UD) fiber reinforced polymer composite is loaded in fiber direction in quasi-...
When a unidirectional (UD) fiber reinforced polymer composite is loaded in fiber direction in quasi-...
When a unidirectional (UD) fiber reinforced polymer composite is loaded in fiber direction in quasi-...
When a unidirectional (UD) fiber reinforced polymer composite is loaded in fiber direction in quasi-...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
The aim of this paper is to analyse fibre/matrix debond crack growth during high stress cyclic tens...
When unidirectional fiber reinforced polymer composites are loaded in tension-tension fatigue multip...
When unidirectional fiber reinforced polymer composites are loaded in tension-tension fatigue multip...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) c...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
The objective of this paper is to analyze fiber/matrix debond crack growth in unidirectional (UD) co...
When a unidirectional (UD) fiber reinforced polymer composite is loaded in fiber direction in quasi-...
When a unidirectional (UD) fiber reinforced polymer composite is loaded in fiber direction in quasi-...
When a unidirectional (UD) fiber reinforced polymer composite is loaded in fiber direction in quasi-...
When a unidirectional (UD) fiber reinforced polymer composite is loaded in fiber direction in quasi-...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
Assuming that Paris law is applicable for individual debond crack propagation along the fiber/matrix...
The aim of this paper is to analyse fibre/matrix debond crack growth during high stress cyclic tens...