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Laminates

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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...
Series: ASM Handbook
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...
Series: ASM Handbook
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...
Series: ASM Handbook
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 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 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 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: 01 January 2001
Fig. 1 Selection of lay-up pattern for fiber-reinforced composite laminates. All fibers in 0°, +45°, 90°, or–45° direction. Note: lightly loaded minimum gage structures tend to encompass a greater range of fiber patterns than indicated, because of the unavailability of thinner plies. More
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Published: 01 January 2001
Fig. 28 Stress-concentration relief at bolt holes in composite laminates More
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Published: 01 January 2001
Fig. 4 Shear buckling coefficient for various graphite/ epoxy laminates More
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Published: 01 January 2001
Fig. 5 Normalized buckling load for [0/90] ns and [90/0] ns laminates as a function of number of ply groups More
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Published: 01 January 2001
Fig. 2 Carpet plots illustrating tensile modulus of laminates More
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Published: 01 January 2001
Fig. 3 Carpet plots illustrating tensile strength of laminates More
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Published: 01 January 2001
Fig. 8 Thermal expansion characteristics of ceramics and carbon-carbon laminates. 2D, two-directional; C/C, carbon-carbon laminae; L , specimen length More
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Published: 01 January 2001
Fig. 13 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 January 2001
Fig. 6 Load distribution in fasteners joining thin and thick laminates More