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Glass fiber-epoxy

Tsai conducted experiments to measure the various moduli of glass-fiber-epoxy-resin composite materials [3-1]. The glass fibers and epoxy resin had a Young s modulus and Poisson s ratio of 10.6 x 10 psi (73 GPa) and. 22 and. 5 x 10 psi (3.5 GPa) and. 35, respectively. [Pg.160]

Fig. 5. Typical DSC-traces for the specific-heat jumps at the glass transition regions of iron-epoxy particulates, or E-glass fiber-epoxy composites and the mode of evaluation of ACp s... Fig. 5. Typical DSC-traces for the specific-heat jumps at the glass transition regions of iron-epoxy particulates, or E-glass fiber-epoxy composites and the mode of evaluation of ACp s...
As soon as the Ar s were determined and the values of r s are found, the values of the adhesion coefficient A may be readily defined by using relation (27). The values of A s for the different fiber-volume contents studied are given in Table II for E-glass fiber-epoxy resin composites with different amounts of fillers, up to 70 percent 22 >. [Pg.178]

Table 2. The values of the characteristic parameters of a series of E-glass fiber, epoxy resin unidirectional composites for various fiber volume contents t>f... [Pg.179]

Fig. 8.7 Examples of hierarchical composites where the presence of CNTs is used for SHM. (a) Damage detection through thermal imaging of resistively-heated CNTs in an alumina composite [47] and (b) detection of crack propagation by monitoring electrical resistance (normalized by specimen length) in a CNT/glass fiber/epoxy composite [48], With kind permission from IOP (2011) and Wiley (2006). Fig. 8.7 Examples of hierarchical composites where the presence of CNTs is used for SHM. (a) Damage detection through thermal imaging of resistively-heated CNTs in an alumina composite [47] and (b) detection of crack propagation by monitoring electrical resistance (normalized by specimen length) in a CNT/glass fiber/epoxy composite [48], With kind permission from IOP (2011) and Wiley (2006).
Fig. 2.7. Spectra of a glass fiber-epoxy matrix composite (a) before and (b) after hydrolysis. After Liao... Fig. 2.7. Spectra of a glass fiber-epoxy matrix composite (a) before and (b) after hydrolysis. After Liao...
Liao, Y.T. (1989). A study of glass fiber-epoxy composite interfaces. Polym. Composites 16, 424-428. Maso, J.C. (1993). Interfaces in Cementitious Composites, E FN Spon, London New York. [Pg.40]

Ikuta, N., Maekawa, Z., Hamada, H, Ichihashi, M. and Nishio, E. (1991). Evaluation of interfacial properties in glass fiber-epoxy resin compositcs-reconsideration of an embedded single filament shear-strength test. J. Mater. Sci. 26, 4663-4666. [Pg.88]

Fig. 5.5. Normalized irKerfacial shear strength of unsized (bare) and sized E-glass fiber-epoxy matrix eomposites measured from the interfaeial testing system (ITS, equivalent to fiber push-out test), short beam shear (SBS) test, 0° flexural test and 90° flexural test. After Drown et al. (1991). Fig. 5.5. Normalized irKerfacial shear strength of unsized (bare) and sized E-glass fiber-epoxy matrix eomposites measured from the interfaeial testing system (ITS, equivalent to fiber push-out test), short beam shear (SBS) test, 0° flexural test and 90° flexural test. After Drown et al. (1991).
Fig. 5.7. Effect of immersion in hot water on interfacial bond strength of silane treated glass fiber-epoxy matrix composite. After Koenig and Emadipotir (1985). Fig. 5.7. Effect of immersion in hot water on interfacial bond strength of silane treated glass fiber-epoxy matrix composite. After Koenig and Emadipotir (1985).
Gershon B. and Marom G. (1975). Fracture toughness and mechanical properties of glass fiber-epoxy composites. J. Mater. Sci. 10, 1549-1556. [Pg.274]

Fig. 8.25. Interlaminar shear strength as a function of stitch density for seven layer off-loom stitched glass fiber-epoxy matrix composites. After Adanur ct al. (1995). Fig. 8.25. Interlaminar shear strength as a function of stitch density for seven layer off-loom stitched glass fiber-epoxy matrix composites. After Adanur ct al. (1995).
Melamine polyphosphate Melapur 200 Ciba (Switzerland) PA66/glass fibers, epoxies, synergistic blends with other flame retardants... [Pg.134]

Consider a unidirectional glass fiber-epoxy matrix laminate. [Pg.694]

Abraham, D. Matthews, S. Mcllhagger, R. A comparison of physical properties of glass fiber epoxy composites produced by wet layup with autoclave consolidation and resin transfer moulding. Compos. Pt. A 1998, 29 (7), 795-801. [Pg.2322]

Aluminum particles were used to reinforce glass fiber/epoxy laminates. The fracture toughness was increased but tensile strength and modulus were decreased. [Pg.737]

The isothermal cure kinetics of a glass fiber-epoxy resin prepreg is investigated using high performance liquid chromatography (HPLC) and differential scanning calorimetry (DSC). The... [Pg.229]

Radford. D.. Ganchev. S.. Qaddoumi. N.. Beauregard. G.. and Zoughi. R. (1994). Millimeter wave nondestructive evaluation of glass fiber epoxy composites subjected to impact fatigue. Proc. of the SPIE. Advanced Microwave and Millimeter-Wave Detectors Conf.. Vol. 2275. [Pg.837]

EUyin F, Martens M. Biaxial fatigue behavior of a multidirectional filament-wound glass-fiber/epoxy pipe. Compos Sci Technol 2001 61(4) 491—502. [Pg.187]

Aluminum alloy Titanium alloy High tensile steel Special glass fiber Epoxy fiberglass Silica Fiber Epoxy carbon fiber Boron fiber Carbon fiber Iron whisker SIC whisker Graphite whisker... [Pg.59]

The first of the fiber-RP materials to be used on Boeing commercial airplanes was the glass fiber/epoxy composition. Boeing has an extensive... [Pg.569]

Hitco Carbon Composites Inc. of Gardena, CA., USA has won a four-year contract to build vapor barrier assemblies for 60 Boeing C-17 aircraft. The autoclaved, foam-cored glass fiber/epoxy panel assembhes measure 6.5 m long by 5.5 m wide (21 ft by 18 ft) with compound curvature, designed to prevent fuel and fuel vapors from the main fuel tanks from penetrating the plane s cargo area. [Pg.582]

Leo Windecker (dentist) builds the Windecker Eagle airplane. The Windecker all-RP airplane, after seven years (1967) of development, is successfully flight tested. It is the first plastic composite to receive USA FAA certification. This glass fiber-epoxy (Dow plastic and construction) plane has a monocoque fuselage. [Pg.589]

Hitco Carbon Composites Inc. of Gardena, CA., USA has won a four-year contract to build vapor barrier assemblies for 60 Boeing C-17 aircraft. The autoclaved, foam-cored glass fiber/epoxy panel... [Pg.591]

Table 7.15 Glass fiber-epoxy RP leaf spring design... Table 7.15 Glass fiber-epoxy RP leaf spring design...
Table 8.1 Data for 3000 psi glass fiber-epoxy spheres... Table 8.1 Data for 3000 psi glass fiber-epoxy spheres...
Walter, T.R., Subhash, G., Sankar, B.V., and Yen, C.F. (2009) Damage modes in 3D glass fiber epoxy woven composites under high rate of impact loading. Composites Part B Engineering, 40, 584—589. [Pg.285]

Figure 12 Stress-strain curve of randomly oriented short glass-fiber/epoxy composites with the maximum strain theory prediction. Figure 12 Stress-strain curve of randomly oriented short glass-fiber/epoxy composites with the maximum strain theory prediction.
Miwa M, Nakayama A, Ohsawa T, Hasegawa A (1979) Temperature dependence of the tensile strength of glass fiber-epoxy and glass fiber-unsaturated polyester composites. J AppI Polym Sci 23 2957... [Pg.288]

See other pages where Glass fiber-epoxy is mentioned: [Pg.73]    [Pg.149]    [Pg.182]    [Pg.236]    [Pg.21]    [Pg.182]    [Pg.287]    [Pg.345]    [Pg.91]    [Pg.229]    [Pg.778]    [Pg.802]    [Pg.578]    [Pg.242]    [Pg.153]    [Pg.161]   
See also in sourсe #XX -- [ Pg.773 ]

See also in sourсe #XX -- [ Pg.773 ]



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