Creep rupture data in Kevlar 49 epoxy usually exhibit considerable scatter: the coefficient of variation (CV) about the mean failure time at a given stress exceeds 100%. Quasi-static strength data, in contrast, shows little scatter: <4% CV for pressure vessels and <10% for impregnated strands. In this paper analysis of existing creep rupture data on Kevlar epoxy vessels at four storage pressures has produced an interesting and useful result. It was found that a significant portion of the scatter in failure times for pressure vessels is due to spool-to-spool variation in the eight spools of Kevlar fibers used to wind the vessels. The order rank of mean times to failure was consistent over a pressure range from 3400 to 4300 psi, 68 to 86% of ...
A study of the stress rupture time of glass fiber epoxy composite laminates in humid environments wa...
Models for the prediction of strength of composite materials are generally directed to short-term fa...
The intrinsic scatter in tensile properties of unidirectional (UD) carbon/epoxy composites is due to...
Long-term behavior of filament-wound pressure vessels were tested, Kevlar 49 epoxy strands were stud...
Lack of long term performance data inhibits the widespread use of composites. The long-term response...
Extensive stress rupture studies on glass composites and Kevlar composites were conducted by the Law...
The wide-spread opinion persists that epoxy matrices behave in a purely brittle manner. Their plasti...
Stress rupture is a failure mechanism where failures can occur after a period of time, even though t...
Composite Overwrapped Pressure Vessel (COPVs) that have survived a long service time under pressure ...
ABSTRACT. Composite Overwrapped Pressure Vessels (COPVs) are frequently used for storing pressurized...
Creep tests at ambient conditions have been carried out on Kevlar 49 and Technora yarns covering a w...
The failure mechanisms of Kevlar&reg; 49 fibers, epoxy resin and uniaxial Kevlar&reg; 49 fib...
For efficient design of pressure components, and cost effective extension of lives of existing compo...
Acoustic emission (AE) data attained during tensile testing of epoxy impregnated Kevlar® 49 (K/Ep) c...
Acoustic emission (AE) data attained during tensile testing of epoxy impregnated Kevlar® 49 (K/Ep) c...
A study of the stress rupture time of glass fiber epoxy composite laminates in humid environments wa...
Models for the prediction of strength of composite materials are generally directed to short-term fa...
The intrinsic scatter in tensile properties of unidirectional (UD) carbon/epoxy composites is due to...
Long-term behavior of filament-wound pressure vessels were tested, Kevlar 49 epoxy strands were stud...
Lack of long term performance data inhibits the widespread use of composites. The long-term response...
Extensive stress rupture studies on glass composites and Kevlar composites were conducted by the Law...
The wide-spread opinion persists that epoxy matrices behave in a purely brittle manner. Their plasti...
Stress rupture is a failure mechanism where failures can occur after a period of time, even though t...
Composite Overwrapped Pressure Vessel (COPVs) that have survived a long service time under pressure ...
ABSTRACT. Composite Overwrapped Pressure Vessels (COPVs) are frequently used for storing pressurized...
Creep tests at ambient conditions have been carried out on Kevlar 49 and Technora yarns covering a w...
The failure mechanisms of Kevlar&reg; 49 fibers, epoxy resin and uniaxial Kevlar&reg; 49 fib...
For efficient design of pressure components, and cost effective extension of lives of existing compo...
Acoustic emission (AE) data attained during tensile testing of epoxy impregnated Kevlar® 49 (K/Ep) c...
Acoustic emission (AE) data attained during tensile testing of epoxy impregnated Kevlar® 49 (K/Ep) c...
A study of the stress rupture time of glass fiber epoxy composite laminates in humid environments wa...
Models for the prediction of strength of composite materials are generally directed to short-term fa...
The intrinsic scatter in tensile properties of unidirectional (UD) carbon/epoxy composites is due to...