n this work, the rate dependence of mode I interlaminar fracture toughness for two different materials systems, IM7/8552 and IM7/M91, both unidirectional UD carbon-fibre epoxy composite laminates have been examined over a wide range of loading rates from 0.5 mm/min up to 2000 mm/s at room temperature. Quasi-static fracture tests were performed using a DCB (double-cantilever beam) method with a screw-driven testing machine, while the dynamic tests were carried out using a WIF (wedge-insert fracture) specimen loaded dynamically in a hydraulic system. For performing the tests at high displacement rates, a special setup was designed and manufactured which allowed the insertion of the wedge within the DCB specimens at different cross-head displa...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.The ...
This paper describes an experimental study involving double cantilever beam (DCB), end-notched flexu...
The Mode I and Mode II fracture behaviour of three carbon-epoxy composite laminates with different f...
In this work, the rate dependence of mode I interlaminar fracture toughness for two different materi...
La relation entre la vitesse de déformation et la résistance à la rupture interlaminaire en Mode II ...
RQsumB: La relation entre la vitesse de deformation et la resistance F la rupture interlaminaire en ...
This paper presents experimental investigations on the in-plane shear behaviour and intralaminar fib...
The design of composite transportation structures with improved crashworthiness behaviour requires a...
A combined numerical-experimental methodology is presented to measure dynamic Mode-I fracture proper...
A combined numerical-experimental methodology is presented to measure dynamic Mode-I fracture proper...
The aim of this research is to understand and analyse the behaviour of specimens used to measure fra...
This paper describes an experimental study developed to characterize the mode I and mode II fractur...
The experimental investigation of fracture toughness under Mode I loading conditions have been perfo...
Testing has been undertaken to study the applicability of linear elastic fracture mechanics to a car...
In the present work, the fracture resistance of a carbon fiber composite under mode I and mode II lo...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.The ...
This paper describes an experimental study involving double cantilever beam (DCB), end-notched flexu...
The Mode I and Mode II fracture behaviour of three carbon-epoxy composite laminates with different f...
In this work, the rate dependence of mode I interlaminar fracture toughness for two different materi...
La relation entre la vitesse de déformation et la résistance à la rupture interlaminaire en Mode II ...
RQsumB: La relation entre la vitesse de deformation et la resistance F la rupture interlaminaire en ...
This paper presents experimental investigations on the in-plane shear behaviour and intralaminar fib...
The design of composite transportation structures with improved crashworthiness behaviour requires a...
A combined numerical-experimental methodology is presented to measure dynamic Mode-I fracture proper...
A combined numerical-experimental methodology is presented to measure dynamic Mode-I fracture proper...
The aim of this research is to understand and analyse the behaviour of specimens used to measure fra...
This paper describes an experimental study developed to characterize the mode I and mode II fractur...
The experimental investigation of fracture toughness under Mode I loading conditions have been perfo...
Testing has been undertaken to study the applicability of linear elastic fracture mechanics to a car...
In the present work, the fracture resistance of a carbon fiber composite under mode I and mode II lo...
Thesis (M.S.)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering.The ...
This paper describes an experimental study involving double cantilever beam (DCB), end-notched flexu...
The Mode I and Mode II fracture behaviour of three carbon-epoxy composite laminates with different f...