Zobrazeno 1 - 10
of 27
pro vyhledávání: '"J. C. SEFERIS"'
Publikováno v:
Journal of Materials Engineering and Performance. 8:661-668
When honeycomb composite structures are fabricated for the aerospace industry, they are designed to be closed to their operating environment for the life of the composite structure. However, once in service, this design can break down. Damage can set
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ffbe5438a2e89c530c22607adfefaed9
https://doi.org/10.1361/105994999770346422
https://doi.org/10.1361/105994999770346422
Publikováno v:
Journal of Applied Polymer Science. 73:505-514
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa84b6c37a70e8152c63b1d2da125069
https://doi.org/10.1002/1097-4628(19990725)73:4<505::aid-app6>3.0.co
https://doi.org/10.1002/1097-4628(19990725)73:4<505::aid-app6>3.0.co
Autor:
J. C. Seferis, D. R. Moore
Publikováno v:
Pure and Applied Chemistry. 69:1153-1162
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ebfae931d72298242fc9f57628bc587a
https://doi.org/10.1351/pac199769051153
https://doi.org/10.1351/pac199769051153
Publikováno v:
Journal of Thermal Analysis. 46:1511-1525
Five epoxy resins of different chemistry and functionality were cured with DDS (4,4′-diaminodiphenyl sulfone) using 2, 8 and 14 h curecycles. Both Differential Scanning Calorimetry (DSC) and Thermomechanical Analysis (TMA) were used to characterize
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3480e43886cf4e84eaeae4d5f3fb000e
https://doi.org/10.1007/bf01980758
https://doi.org/10.1007/bf01980758
Publikováno v:
Science and Engineering of Composite Materials, Vol 4, Iss 3, Pp 143-154 (1995)
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::53ea8138c8a056899c0529f90ddb2527
https://doaj.org/article/ba94db8e16c8498a96efe7dedcedfea3
https://doaj.org/article/ba94db8e16c8498a96efe7dedcedfea3
Publikováno v:
Journal of Thermal Analysis. 42:467-484
This investigation demonstrates that polyphenylene sulfide (PPS) crystallizes in a unique dual-mechanistic fashion in which 8% of the material by volume crystallizes instantaneously, while the remaining material crystallizes in a time dependent fashi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::874aa0ec79be194aa4d2721f6aaa8eb1
https://doi.org/10.1007/bf02548529
https://doi.org/10.1007/bf02548529
Autor:
Kyujong Ahn, J. C. Seferis
Publikováno v:
Polymer Composites. 14:349-360
A description of the hot-melt prepreg process was developed by coupling resin matrix flow at the coating and impregnation zones with heat transfer considerations. Both bismaleimide (BMI) and epoxy resin systems were used as matrices. With continuous
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::28ce64f5a0cefe441fd70359e6fc5a5e
https://doi.org/10.1002/pc.750140411
https://doi.org/10.1002/pc.750140411
Autor:
J. C. Seferis, Chris N. Velisaris, George C. Papanicolaou, Vasileios M. Drakonakis, Charalambos C. Doumanidis, Brian L. Wardle
Publikováno v:
Wardle (via assistant)
Polymeric composites have gone through a level of maturity beyond the laboratory stage with the development of the Boeing 787, the structure of which contains more than 50% composites. Nonetheless, a basic understanding of the material used in its pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::37cbeecb96330c1555a83eeb712f2e30
https://orcid.org/0000-0003-3530-5819
https://orcid.org/0000-0003-3530-5819
Publikováno v:
Polymer Composites. 13:197-206
As part of an engineering analysis and experimental methodology to characterize prepreg tack, a compression-to-tension test was optimized to enhance reproducibility and generate intrinsic property data. With the resulting stress-strain compression an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d7262b6e6093f1d4426f15f4835b7778
https://doi.org/10.1002/pc.750130308
https://doi.org/10.1002/pc.750130308
Publikováno v:
Journal of Applied Polymer Science. 45:399-406
Thermoanalytical measurements and tack tests were both performed using a commercially available carbon fiber/epoxy prepreg system (Hercules 3501–6) to examine changes caused by aging as they affect handling and processability of thermosetting matri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6137ee83630f5f1f3a5728e089f1bdbe
https://doi.org/10.1002/app.1992.070450304
https://doi.org/10.1002/app.1992.070450304