Science and Technology of Fibers and Related Materials: Proceedings of the Fiber Society 50th Anniversary Technical Conference Held in Princeton, New Jersey, August 19-23, 1990 |
From inside the book
Results 1-3 of 19
Page 499
For example , flexural strength was compared for a traditional laminated braided
preform and a multilayer interlock braided preform . Kevlar 49 ( 1420 den ) was
braided at orientation angle of + 63o . Both structures had five layers of braid and
...
For example , flexural strength was compared for a traditional laminated braided
preform and a multilayer interlock braided preform . Kevlar 49 ( 1420 den ) was
braided at orientation angle of + 63o . Both structures had five layers of braid and
...
Page 503
3 - D BRAIDED PREFORMS The 3 - D braiding technology is an extension of the
well established 2 - D braiding technology wherein the fabric is constructed by
the intertwining or orthogonal interlacing of two or more yarn systems to form an ...
3 - D BRAIDED PREFORMS The 3 - D braiding technology is an extension of the
well established 2 - D braiding technology wherein the fabric is constructed by
the intertwining or orthogonal interlacing of two or more yarn systems to form an ...
Page 512
An observation of the failure mode of the OHT and OHC specimens reveals that ,
although the laminated composites had higher strength , the 3 - D braided
composites contain damage better . In laminated composites , the predominant
mode ...
An observation of the failure mode of the OHT and OHC specimens reveals that ,
although the laminated composites had higher strength , the 3 - D braided
composites contain damage better . In laminated composites , the predominant
mode ...
What people are saying - Write a review
We haven't found any reviews in the usual places.
Contents
M | 33 |
Strain Rate Effects in Ultrastrong Polyethylene Fibers and Composites | 45 |
Morphology and Near Tm Behavior of High Performance Ultrahigh | 67 |
Copyright | |
30 other sections not shown
Common terms and phrases
amorphous analysis angle appearance Applied behavior bending blend body braided break calculated carpet cellulose compared composite compression constant cotton crystalline crystallization curve decrease deformation density dependence described determined developed diameter direction discussed distance distribution draw effect elastic energy experimental extension fabric factor failure fiber Figure filament finish force frictional function geometry given heat higher improved increase indicated initial length liquid load lower m/min material measured mechanical method modulus nylon observed obtained occurs orientation parameter polyester polymer present pressure problem produced properties range ratio reduced relative resistance sample scanning shape shear shown in Figure shows solution specimen speed spinning spun strain strength stress structure surface Table temperature tenacity tensile tension Text treated treatment twist unit untreated values variability yarn