| 1. | Carbon filament cloth
碳丝织物 |
| 2. | Aerospace ; preimpregnated woven fabric of carbon filament yarn and epoxy resin ; technical specification
航空航天.预浸渍的碳纤维长丝织物和环氧树脂.技术规 |
| 3. | Aerospace ; reinforcement fibres ; determination of size content of carbon filament yarns , woven fabrics and chopped strands
航空航天.增强纤维.碳素长丝纱织物和短切原丝的浆 |
| 4. | Aerospace ; reinforcement fibres ; determination of thermal oxidative resistance of carbon filament yarns , woven fabrics and short cuts
航空航天.增强纤维.碳素长丝纱织物和短切原丝的耐 |
| 5. | Aerospace ; reinforcement fibres ; qualitative determination of size constituents of carbon filament yarns , woven fabrics and chopped strands by hplc
航空航天.增强纤维.用hplc法对碳素长丝纱织物和短 |
| 6. | Aerospace ; reinforcement fibres ; qualitative testing of size type of carbon filament yarns , woven fabrics and chopped strands by infrared spectroscopy
航空航天.增强纤维.用红外分光法对碳素长丝纱织物 |
| 7. | Tensile tests of carbon filament yarn shows at high strain rate that the mechanical behavior of carbon fiber bundles are insensitive to strain rate , i . e . , the failure stress strain and elastic modulus are not increased with the rising of strain - rate . however , the fractograph of carbon fiber is rate - dependent . the fractograph of carbon will become smooth from coarse as the strain rate increases
通过对碳纤维束的冲击拉伸试验表明，虽然碳纤维束的力学性能与应变率基本上是不相关的，即随着应变率的增大，碳纤维束的初始模量、破坏应力及其失效应变都变化不大，但碳纤维束的破坏断口与冲击拉伸实验的应变率密切相关。 |
