Thesis (Ph.D.)--University of Washington, 2017-08Composite materials are widely used in various industries for making structural parts due to higher strength to weight ratio, better fatigue life, corrosion resistance and material property tailorability. To fully exploit the capability of composites, it is required to know the load carrying capacity of the parts made of them. Unlike metals, composites are orthotropic in nature and fails in a complex manner under various loading conditions which makes it a hard problem to analyze. Lack of reliable and efficient failure analysis tools for composites have led industries to rely more on coupon and component level testing to estimate the design space. Due to the complex failure mechanisms, compos...
This is an Open-Access article distributed under the terms of the Creative Commons Attribution Non-C...
A computational simulation tool is used to evaluate the various stages of damage progression in comp...
Bachelor thesis deals with possibilities of progressive failure analysis of layered composite plates...
Predicting the failure of materials is one of the oldest problems in engineering and one of the leas...
Introduction. Composite laminate failure progression is a wide and complex problem that is studied c...
ABSTRACT: Recent developments in the aircraft industry towards substantially improving fuel economy ...
Taking advantage of major recent advances in computational methods and the conceptual representation...
This paper is concerned with a progressive failure analysis methodology for fiber reinforced composi...
Aircraft composite structures must have high stiffness and strength with low weight, which can guara...
This thesis presents the Progressive Failure Analysis (PFA) to enhance the design of the composite s...
In the design of bonded aircraft structures, the type of failure is crucial. More specifically, the ...
Various failure modes can occur in a composite laminate subjected to external load. With the increas...
Success with the high strain rate testing of polymer composites has been limited by the ability to i...
The aerospace industry is committed to improve the performance of aircraft whilst reducing emissions...
Woven polymer-based composites are currently used in a wide range of naval applications. Use of comp...
This is an Open-Access article distributed under the terms of the Creative Commons Attribution Non-C...
A computational simulation tool is used to evaluate the various stages of damage progression in comp...
Bachelor thesis deals with possibilities of progressive failure analysis of layered composite plates...
Predicting the failure of materials is one of the oldest problems in engineering and one of the leas...
Introduction. Composite laminate failure progression is a wide and complex problem that is studied c...
ABSTRACT: Recent developments in the aircraft industry towards substantially improving fuel economy ...
Taking advantage of major recent advances in computational methods and the conceptual representation...
This paper is concerned with a progressive failure analysis methodology for fiber reinforced composi...
Aircraft composite structures must have high stiffness and strength with low weight, which can guara...
This thesis presents the Progressive Failure Analysis (PFA) to enhance the design of the composite s...
In the design of bonded aircraft structures, the type of failure is crucial. More specifically, the ...
Various failure modes can occur in a composite laminate subjected to external load. With the increas...
Success with the high strain rate testing of polymer composites has been limited by the ability to i...
The aerospace industry is committed to improve the performance of aircraft whilst reducing emissions...
Woven polymer-based composites are currently used in a wide range of naval applications. Use of comp...
This is an Open-Access article distributed under the terms of the Creative Commons Attribution Non-C...
A computational simulation tool is used to evaluate the various stages of damage progression in comp...
Bachelor thesis deals with possibilities of progressive failure analysis of layered composite plates...