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Carbon epoxy specific heat

Of interest is the study of the properties of glass-carbon fibres on the basis of epoxy resin EDT-10 with modifying additives as well as of the filler composed of carbon and glass fibre ropes in a temperature range between 10 and 400 K. In Fig. 3, specific heat (J/kg K), thermal conductivity (W/m K) and thermal diffusivity (m /s) of glass-carbon fibres along (il) and across (j.) the fibres are plotted against temperature. Temperature dependences A ) (T),... [Pg.310]

At RT, thermal conductivities of carbon fiber composites with high tensile fibers differ from those of high modulus fibers and are much higher than the thermal conductivity of the epoxy matrix. Below 7 K, they become similar within 25% and lower than the thermal conductivity of the epoxy matrix (37,47). The similarity is owing to the fact that at low temperatures only long phonon wavelengths are activated they cannot resolve different graphite microstructures of different carbon fiber types which are dominant at RT (36,43). In most cases, the specific heat of composites is lower than that of the polymeric matrix. [Pg.168]

Shipment and Storage, Specifications. A/-Vinyl-2-pyrrohdinone is available in tank cars and tank trailers and in dmms of various sizes. Shipping containers are normally steel or stainless steel. Tank cars are provided with heating coils to facihtate unloading in cold weather. Rubber, epoxy, and epoxy—phenohc coatings are attacked and must be avoided. Carbon steel has been successfully used for storage tanks, but stainless steel preserves product quahty better. Aluminum and certain phenohc coatings are also satisfactory. [Pg.523]

As shown in the previous section, most polymer composites used in construction involve highly flammable matrices, such as polyester, vinylester or epoxy resins. Besides, if glass and carbon fibres are generally considered heat resistant, other type of fibres used for specific applications may also exhibit poor fire behaviour (aramid, polyolefins or other polymer fibres, for instance). Therefore, to meet the safety requirements specified in building codes and... [Pg.423]

Gilman et al. found similar reductions in the PHRR of clay nanocomposites. They prepared 6 wt% intercalated nanocomposites with Cloisite 15A dispersed in a nitrile rubber-modified bisphenol A epoxy-based vinyl ester (mod-bis-A) or a combination of bisphenol A and novolac epoxy-based vinyl ester (bis-A/novolac). The PHRR was reduced by 25 and 39% for mod-bis-A and bis-A/novolac, respectively. The clay promoted charring in fact, no residue was obtained for the neat resins, while in the nanocomposites the residue yields were 8 wt% (mod-bis-A) or 9 wt% (bis-A/novolac). The heat of combustion, specific extinction area, and carbon monoxide yields were unchanged. [Pg.276]


See other pages where Carbon epoxy specific heat is mentioned: [Pg.99]    [Pg.841]    [Pg.620]    [Pg.535]    [Pg.773]    [Pg.1206]    [Pg.507]    [Pg.272]    [Pg.464]    [Pg.271]    [Pg.139]    [Pg.150]    [Pg.796]    [Pg.374]    [Pg.337]    [Pg.153]    [Pg.337]    [Pg.251]    [Pg.534]    [Pg.617]    [Pg.91]    [Pg.419]    [Pg.207]    [Pg.29]   
See also in sourсe #XX -- [ Pg.162 ]




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