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Book Chapter
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003383
EISBN: 978-1-62708-195-5
... describes the damping characteristics of unidirectional composites, when they are subjected to longitudinal shear, longitudinal tension/compression, and transverse tension/compression. It presents equations that govern the overall damping capacity of beams that are cut from laminated plates. The article...
Abstract
Damping is the energy dissipation properties of a material or system under cyclic stress. The vibrational and damping characteristics of composites are important in many applications, including ground-based and airborne vehicles, space structures, and sporting goods. This article describes the damping characteristics of unidirectional composites, when they are subjected to longitudinal shear, longitudinal tension/compression, and transverse tension/compression. It presents equations that govern the overall damping capacity of beams that are cut from laminated plates. The article discusses the effect of temperature on damping and provides information on the relationship between damping and strength.
Image
Published: 01 January 1987
Fig. 1008 Tension-overload fracture in the short-transverse plane of a specimen of aluminum alloy 7075-T6. At top and bottom are regions of quite small dimples. In the central portion of this view are large pockets in which the cleaved facets of intermetallic inclusions are visible
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Image
Published: 01 June 2024
Fig. 9 Tension overload fracture in short-transverse plane of a 7075-T6 alloy. Large pockets with intermetallic inclusions, rich in iron and silicon, are visible. SEM; original magnification: 80×. Source: Ref 5
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Image
Published: 01 August 2018
Fig. 16 Area plot of acoustic emission (AE) count rate versus strain. (a) Longitudinal tension test of a B(B 4 C) fiber-reinforced Ti-6Al-4V metal-matrix composite (MMC) specimen. (b) Transverse tension test of a B(B 4 C) fiber-reinforced Ti-6Al-4V MMC specimen. (c) Transverse tension test
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Book Chapter
Book: Fractography
Series: ASM Handbook Archive
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000625
EISBN: 978-1-62708-181-8
... the ductile fracture, interlaminar failure, transgranular cleavage and fracture, tension-overload fracture, longitudinal and transverse cracking, fiber splitting, stress rupture, and low-cycle fatigue of these composites. ductile to brittle transition fractograph metal-matrix composites tensile...
Abstract
This article is an atlas of fractographs that helps in understanding the causes and mechanisms of fracture of metal-matrix composites, including tungsten fiber-reinforced aluminum, tungsten fiber-reinforced carbon steel, and tungsten fiber-reinforced silver. The fractographs illustrate the ductile fracture, interlaminar failure, transgranular cleavage and fracture, tension-overload fracture, longitudinal and transverse cracking, fiber splitting, stress rupture, and low-cycle fatigue of these composites.
Image
Published: 01 January 1987
Fig. 1260 Fracture due to fiber splitting in tungsten fiber reinforced metal-matrix composites. When the tungsten/aluminum and tungsten/steel composites in Fig. 1255 , 1256 , 1257 , 1258 , and 1259 fractured under transverse tension loading, the predominant failure mode was fiber
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Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003379
EISBN: 978-1-62708-195-5
... of elasticity of the fiber, and E m is the modulus of elasticity of the matrix. Subscripts f, m, L, and T refer to fiber, matrix, longitudinal, and transverse, respectively. At the pure transverse tension case, in the absence of longitudinal stress, a typical amplification factor, R , between...
Abstract
This article presents a comprehendable and comprehensive physics-based approach for characterizing the strength of fiber-reinforced polymer composites. It begins with background information on the goals and attributes of this method. The article then addresses the characterization of fiber failures in laminates, because these are at the highest strengths that can be attained and, therefore, are usually the design objective. An exception would be if the design goal is to maximize energy absorption, rather than static strength. The discussion proceeds to situations in which the matrix fails first, either by intent, by design error, or because of impact damage. The state of the modeling propagation and arrest of matrix damage follows. Comparisons of this physics-based approach are then made to empirically based failure theories.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003444
EISBN: 978-1-62708-195-5
... of Hoop Wound Polymer Matrix Composite Cylinders Transverse tension D 5467 Compressive Properties of Unidirectional Polymer Matrix Composites Using a Sandwich Beam In-plane compression D 5766/D 5766M Open Hole Tensile Strength of Polymer Matrix Composite Laminates Open-hole tensile strength...
Abstract
This article explores why structural element and subcomponent testing are conducted. It discusses the different types of failure modes in composites, and provides information on the testing methodology, fixturing, instrumentation, and data reporting. The article reviews various standard elements used to characterize composite materials for the various failure modes. Simple structural-element testing under in-plane unidirectional, multidirectional, and combined loading, as well as out-of-plane loading are discussed. Simple bolted and bonded joints, as well as data correlation are reviewed with analytical predictions. The article also provides a list of the ASTM testing standards applicable at the element level of testing for both polymer-matrix composites and metal-matrix composites. It concludes with a discussion on durability and damage tolerance testing.
Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001474
EISBN: 978-1-62708-173-3
.../AWS B4.0. Fig. 6 Tension and bend specimens for testing of full-penetration groove welds. (a) Reduced-section tension specimen. (b) Round tension specimen. (c) Bend specimen Transverse Tension Tests Transverse tension tests are performed on full-penetration groove welds to determine...
Abstract
Welding codes and standards usually require the qualification of welding procedures prior to being used in production. This is to ensure that welds will meet the minimum quality and mechanical property requirements for the application. This article provides an overview of the welding procedure qualification guidelines and test methods. It also reviews the codes, standards, and specifications that govern the design and fabrication of welded structures for the procedure qualification details that are appropriate for a given application.
Image
Published: 01 January 1996
Fig. 39 Influence of texture on fatigue crack growth in Ti-6Al-4V. Fatigue crack growth rates are higher when basal planes are loaded in tension. The elastic modulus in tension for the basal texture (B) is 109 GPa; for the transverse texture (T), 126 GPa. The yield stress is roughly 1150 MPa
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Book Chapter
Book: Composites
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
... of temperature and moisture through the thickness of a laminate. Stresses caused due to mechanical loads, temperature, and moisture on the laminate are analyzed. The article concludes with information on interlaminar cracking, free-edge delamination, and transverse cracks of laminates. unidirectional...
Abstract
The properties of unidirectional composite (UDC) materials are quite different from those of conventional, metallic materials. This article provides information on the treatment of UDC stress-strain relations in the forms appropriate for analysis of thin plies of material. It explains 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 of temperature and moisture through the thickness of a laminate. Stresses caused due to mechanical loads, temperature, and moisture on the laminate are analyzed. The article concludes with information on interlaminar cracking, free-edge delamination, and transverse cracks of laminates.
Image
Published: 01 January 2000
Fig. 4 Effect of stress concentrations in tension. (a) No stress concentration. (b) Surface stress concentrations. (c) Transverse hole stress concentration.
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Image
Published: 01 January 2001
Fig. 41 Experimental (shaded) and simulated (points) transverse crack density versus laminate tension relations. Data from four [0° 2 /90°] s coupons
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Image
Published: 01 January 2001
Fig. 42 Experimental (shaded) and simulated (points) transverse crack density versus laminate tension relations. Data from four [0° 2 /90° 2 ] s coupons
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Image
Published: 01 January 2001
Fig. 43 Experimental (shaded) and simulated (points) transverse crack density versus laminate tension relations. Data from four [0° 2 /90° 4 ] s coupons
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Book Chapter
Book: Fractography
Series: ASM Handbook Archive
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000629
EISBN: 978-1-62708-181-8
... no further weight loss was detected. They were tested in a dry oven at the temperatures noted.)(L. Clements, San Jose State University, and J.C. Liu, Cornell University) Fig. 1296 Fracture surface of a transverse (90°) carbon/epoxy specimen that failed in tension. The specimen was tested in the dry...
Abstract
This article is an atlas of fractographs that helps in understanding the causes and mechanisms of fracture of a type of resin-matrix composites, carbon-epoxy composites. The fractographs illustrate the fracture modes found in composite prepregs, composite panels, solid rocket motor nozzles, and tension, flexural, compressive, and shear loadings.
Image
Published: 15 June 2019
Fig. 45 Crack growth comparison. Many commercial aluminum alloys show similar fatigue crack propagation rates in air, as indicated above. L-T, longitudinal transverse; CNP, center-notch panel; DCB, double-cantilever beam; CT, compact tension. Source: Ref 90
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Image
Published: 01 January 1987
Fig. 1271 Surface of a tension-overload fracture in a composite consisting of tungsten fibers in a silver matrix. The tungsten fiber marked P has undergone a ductile fracture with necking, whereas fiber Q has suffered a sharp, flat, transverse cleavage fracture. See also Fig. 1272 . SEM, 320×
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Image
Published: 01 January 2003
Fig. 16 Mean breaking stress versus exposure time for short-transverse 3.2 mm (0.125 in.) diam aluminum alloy 7075 tension specimens tested according to ASTM G 44 at various exposure stress levels. Each point represents an average of five specimens. Source: Ref 3
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Image
Published: 01 January 2003
Fig. 42 Effect of variations in atmospheric environment on the probability and time to failure by SCC of a material with an intermediate susceptibility. Tests were made on short-transverse 3.2 mm (0.125 in.) diam tension specimens from 7075-T7651 type plate stressed 310 MPa (45 ksi
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