There are few if any clear, visual, and detailed images of carbon fiber strand failures under tension useful for determining mechanisms, sequences of events, different types of failure modes, etc. available to researchers. This makes discussion of physics of failure difficult. It was also desired to find out whether the test article-to-test rig interface (grip) played a part in some failures. These failures have nothing to do with stress rupture failure, thus representing a source of waste for the larger 13-00912 investigation into that specific failure type. Being able to identify or mitigate any competing failure modes would improve the value of the 13-00912 test data. The beginnings of the solution to these problems lay in obtaining imag...
Develop and demonstrate NDE techniques for real-time characterization of CPVs and, where possible, i...
In August of 1999, Boeing Corporation (Boeing) engineers began investigating failures of optical fib...
The reliability of impact simulations for aircraft components made with triaxial-braided carbon-fibe...
Recent advancements in braiding technology have led to commercially viable manufacturing approaches ...
Various experimental and analytical studies performed for the NASA carbon fiber risk assessment prog...
A study was initiated to determine the root cause of failure for circuit board electrical connection...
The scope and status of the effort to assess the risks associated with the accidental release of car...
Failure mechanisms in carbon-epoxy composites are identified as a basis for more reliable prediction...
Static 3-point bend tests of Reinforced Carbon-Carbon (RCC) were conducted to failure to provide dat...
The risks associated with the use of carbon fiber composites in civil aircraft are discussed along w...
The potential hazard to electrical and electronic devices should there be a release of free carbon f...
Carbon fibers released from composites by aircraft fires and crashes can cause electrical shorts and...
An efficient method for detecting carbon fibers collected on a stick tape monitor was developed. The...
A series of tests was conducted to measure the strength of stitched carbon/epoxy composites containi...
The stress rupture strength of silicon carbide fiber-reinforced silicon carbide composites with a bo...
Develop and demonstrate NDE techniques for real-time characterization of CPVs and, where possible, i...
In August of 1999, Boeing Corporation (Boeing) engineers began investigating failures of optical fib...
The reliability of impact simulations for aircraft components made with triaxial-braided carbon-fibe...
Recent advancements in braiding technology have led to commercially viable manufacturing approaches ...
Various experimental and analytical studies performed for the NASA carbon fiber risk assessment prog...
A study was initiated to determine the root cause of failure for circuit board electrical connection...
The scope and status of the effort to assess the risks associated with the accidental release of car...
Failure mechanisms in carbon-epoxy composites are identified as a basis for more reliable prediction...
Static 3-point bend tests of Reinforced Carbon-Carbon (RCC) were conducted to failure to provide dat...
The risks associated with the use of carbon fiber composites in civil aircraft are discussed along w...
The potential hazard to electrical and electronic devices should there be a release of free carbon f...
Carbon fibers released from composites by aircraft fires and crashes can cause electrical shorts and...
An efficient method for detecting carbon fibers collected on a stick tape monitor was developed. The...
A series of tests was conducted to measure the strength of stitched carbon/epoxy composites containi...
The stress rupture strength of silicon carbide fiber-reinforced silicon carbide composites with a bo...
Develop and demonstrate NDE techniques for real-time characterization of CPVs and, where possible, i...
In August of 1999, Boeing Corporation (Boeing) engineers began investigating failures of optical fib...
The reliability of impact simulations for aircraft components made with triaxial-braided carbon-fibe...