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Book Chapter

Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002415
EISBN: 978-1-62708-193-1
... Abstract Knowledge of fatigue behavior at the laminate level is essential for understanding the fatigue life of a laminated composite structure. This article describes fatigue failure of composite laminates in terms of layer cracking, delamination, and fiber break and interface debonding...
Book Chapter

By Rod Wishart
Series: ASM Handbook Archive
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003443
EISBN: 978-1-62708-195-5
... Abstract This article provides the general mechanical testing guidelines for the characterization of lamina and laminate properties. Guidelines are provided for tensile property, compressive property, shear property, flexure property, fracture toughness, and fatigue property test methods...
Book Chapter

Series: ASM Handbook Archive
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003378
EISBN: 978-1-62708-195-5
... the development of the relations between mid-surface strains and curvatures and membrane stress and moment resultants. The article discusses the properties, such as thermal expansion, moisture expansion, and conductivity, of symmetric laminates and unsymmetric laminates. It describes the distribution...
Book Chapter

By John Moylan
Series: ASM Handbook Archive
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003442
EISBN: 978-1-62708-195-5
... of thermal expansion and coefficient of moisture expansion; glass transition temperature; thermal conductivity, diffusivity, and specific heat. lamina nonmechanical testing laminate nonmechanical testing nonmechanical properties composite materials ply thickness density coefficient of thermal...
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Published: 01 January 1994
Fig. 2 Thermal expansion characteristics of ceramics and carbon-carbon laminates. C/C, carbon-carbon laminate; L , specimen length More
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Published: 01 January 1996
Fig. 48 Fatigue crack growth in laminates of β-21S at various temperatures between 23–760 °C. (a) da / dN -ΔK curves. (b) Data at 23–482 °C plotted as da / dN vs. (Δ K ) 2 / E σ y . The correlation using the CTOD-like parameter is good for the bcc β phase. Source: Ref 96 More
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Published: 01 January 1996
Fig. 6 S-N curves for (a) various AS4-epoxy laminates and (b) glass-fiber polymer laminates at various ply orientations. Source: (a) Engineered Materials Handbook, Vol 1, Composites, ASM International, 1987, p 438 and (b) C. Osgood, Fatigue Design, 2nd ed., 1982, Pergamon Press, p 530 More
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Published: 01 January 1996
Fig. 13 Fiber-metal laminates structure, a standard 3/2 lay-up: three layers of aluminum, two layers of prepreg. Source: Ref 27 More
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Published: 01 January 1996
Fig. 6 Damage diameter for [45/0/−45/90] 6s IM7/8551-7 and AS4/3501-6 laminates with 12.7 mm diam indenter More
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Published: 01 January 1996
Fig. 24 Constant amplitude compression fatigue for [45/0/−45/90] 6s laminates with impact damage resulting in 2.54 mm dent More
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Published: 01 January 1996
Fig. 31 R-curves for [ + 45/0/90/ + 30/ 0 ] s AS4/938 fuselage crown laminates with various cut lengths. W ≥ 8 a o More
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Published: 01 January 2000
Fig. 38 Fiber bridging in DCB testing of unidirectional laminates More
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Published: 01 November 1995
Fig. 13 Thermal expansion characteristics of ceramics and carbon-carbon laminates. 2D, two-directional; C/C, carbon-carbon laminate; L , specimen length More
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Published: 01 November 1995
Fig. 18 Coefficient of thermal expansion, parallel and perpendicular to laminates of two-directional weave carbon-carbon composite with final heat treatment temperature (HTT) of 1200 and 2400 °C (2190 and 4350 °F) More
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Published: 01 November 1995
Fig. 35 Tensile modulus of elasticity of carbon-epoxy laminates at room temperature More
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Published: 01 November 1995
Fig. 36 Ultimate tensile strength of carbon-epoxy laminates at room temperature More
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Published: 01 August 2018
Fig. 36 Relative sensitivity of instruments used to inspect bonded laminates of increasing total thicknesses. A, Sondicator, contact method; B, Shurtronics harmonic bond tester; C, Fokker bond tester; D, NDT-210 bond tester; E, Sondicator, through-transmission method; F, ultrasonic pulse echo More
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Published: 15 May 2022
Fig. 1 Percent gains in weight of ASTM C581 laminates of a high- and low-styrene-containing vinyl ester exposed at 66 °C (150 °F) to a distilled and saturated sodium chloride solution for 120 days More
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Published: 15 May 2022
Fig. 16 Degradation of glass laminates in water at 100 °C (212 °F) for different polyester-resin matrices. BPA, bisphenol A More
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Published: 01 January 1997
Fig. 4 Fiber arrangements. Composite laminates are generally fabricated by rotating lamina axes as shown by the twist example on the left. However, loads that are off-fiber axes cause large inter- and intralaminar matrix stresses. Safer structures can often be designed by using curved More