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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 1990
Fig. 15 Tension-tension fatigue curves for longitudinal specimens of air-melted and electroslag-remelted heats of H13 steel. Axial fatigue tests performed in an Ivy machine at a frequency of 60 Hz; the alternating stress was 67% of the mean stress for all tests ( R = 0.2). Arrows signify
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Image
Published: 01 January 1987
Fig. 919 Longitudinal section through a tension fracture in a warp wire of a Fourdrinier wire cloth of phosphor bronze C. Slip lines are visible throughout the microstructure. Plastic flow and reduction in area at the fracture (top) were attributed to excessive warp tension, FeCl 3 etch, 265×
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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.
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.
Image
Published: 15 June 2019
Fig. 51 Fatigue crack propagation data for 7050-T7452 hand forgings. L-T, longitudinal transvers; S-L, short longitudinal; CT, compact tension. Source: Ref 99
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Image
Published: 01 January 1996
Fig. 14 Microstructure of compact tension specimens from type 316 piping. (a) Stringers aligned in axial direction. (b) Longitudinal-circumferential (L-C) orientation. Extensive plastic deformation and deep microvoids nucleated by stringers. (c) Circumferential-longitudinal (C-L) orientation
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Image
Published: 01 January 1987
of fatigue”) on a longitudinal shear plane and progressed alternately on 45° tension planes and longitudinal shear planes, as indicated in the diagram. Note that the semicircular fatigue patch surrounding the origin lies in the 45° plane. 1.25×
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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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Series: ASM Handbook
Volume: 14B
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v14b.a0005103
EISBN: 978-1-62708-186-3
... length. Longitudinal Corrugation Longitudinal corrugation ( Fig. 7 ) is a longitudinal condition similar to transverse bow except that the sense of the curvature changes sign at least once across the width of the metal. Corrugation is usually caused by application of excessive tension, to which...
Abstract
Metal production mills produce flat metal sheet and strip products into coil forms that are subjected to further fabrication for shape correction. This article provides a discussion on the principle of shape correction and describes the role of various fabrication processes in shape correction. These processes include flattening, leveling, slitting, and cut-to-length.
Image
Published: 01 January 2000
Fig. 7 Typical stress-strain curves in tension for wrought Ti-6Al-4V. (a) Annealed extrusions. Static strain rate, after 1 2 h exposure. (b) All product forms, solution treated and aged (STA), longitudinal direction, after 1 2 h exposure. Source: Ref 6
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Image
Published: 01 January 2000
Fig. 3 Elevated-temperature stress-strain curves in tension for Fe-18Cr-8Ni (Type 301) stainless steel. (a) 0.508 mm (0.020 in.) sheet full hard from 40% reduction (data average of longitudinal and transverse). (b) 0.813 mm (0.032 in.) sheet full hard with stress relief at 425 °C (800 °F
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Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003046
EISBN: 978-1-62708-200-6
... laminate with a 0° ply bonded to each surface on each end but terminating near the center of the specimen. Tension load was applied. The control specimen with the terminating plies cut off straight and perpendicular to the longitudinal axis failed at 77% of the parent allowable by the peeling away...
Abstract
Relatively limited effort has gone into developing repair processes and materials for composites, in contrast to the significant labor and expense that has gone into the development of these materials for numerous critical applications. As composites gain wider acceptance as aerospace materials, there is a need to understand the requirements of the end users regarding repair of these advanced materials. This article focuses on the repair of graphite-epoxy structures designed in a variety of forms for a wide range of load intensities. Five repair concepts developed for generic laminate repair have been validated in this article through the required environmental and load condition tests. These include bonded-scarf joint flush repair, double-scarf joint flush repair, blind-side banded-scarf repair, blind-side sandwich repair, and bonded external patch repair. A brief note on thermoplastic repair concepts is also provided in this article.
Image
Published: 01 January 1990
Fig. 16 Tension-compression fatigue curves for air-melted and electroslag-remelted heats of H13 steel. Axial fatigue tests performed in an Ivy machine at a frequency of 60 Hz; the stresses were fully reversed for all tests ( R = −1). Open symbols indicate longitudinal fatigue data; filled
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Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003325
EISBN: 978-1-62708-176-4
... are described in AWS B4.0 for two orientations of fillet welds (transverse to the tension loading and longitudinal to the tension loading) ( Ref 8 , 9 ). The transverse specimen is a double lap specimen with loaded fillet welds, as shown in Fig. 1 . The longitudinal specimen is a combination of two lapped...
Abstract
This article discusses the standard test methods that can be applied to many types of welds: tension, bending, impact, and toughness testing. It provides information on four qualification stages, namely, the weld material qualification, base material qualification, the weld procedure qualification, and the weld service assessment. The article describes two general types of measurements for residual stress in welds: locally destructive techniques and nondestructive techniques. Locally destructive techniques include hole drilling, chip machining, and block sectioning. Nondestructive techniques include X-ray diffraction, neutron diffraction, Barkhausen noise analysis, and ultrasonic propagation analysis. The article concludes with an overview of weldability testing.
Image
Published: 15 June 2020
Fig. 1 Three-bar analogy illustrating the formation of residual stresses during welding, also applicable to understanding additive manufacturing residual stress. Outer bars represent the surface longitudinal component on which material is deposited, center bar represents the weld region, blue
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Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003374
EISBN: 978-1-62708-195-5
... or molecule on the surface of a liquid or a solid has a net force acting on it, pulling it toward the interior of that phase. The manifestation of this force is commonly called the surface tension (also called “surface energy”). In a liquid where the rearrangement of molecules takes place on the microsecond...
Abstract
Fiber-matrix adhesion is a variable to be optimized in order to get the best properties and performance in composite materials. This article schematically illustrates fiber matrix interphase for composite materials. It discusses thermodynamics of interphase in terms of surface energy, contact angle, work of adhesion, solid surface energy, and wetting and wicking. The article describes the change in interphase depending on the reinforcing fiber such as glass fiber, polymeric fiber, and carbon fiber. It emphasizes fiber-matrix adhesion measurements by direct methods, indirect methods, and composite laminate tests. The effects of interphase and fiber-matrix adhesion on composite mechanical properties, such as composite on-axis properties, composite off-axis properties, and composite fracture properties, are also discussed.
Image
Published: 01 January 2002
Fig. 15 Titanium heat-exchanger tube (ASTM B337, grade 2) that became embrittled and failed because of absorption of hydrogen and oxygen at elevated temperatures. (a) Section of the titanium tube that flattened as a result of test per ASTM B 337; the first crack was longitudinal along the top
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Image
in Failure Analysis of Heat Exchangers
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 16 Titanium heat-exchanger tube (ASTM B337, grade 2) that became embrittled and failed because of absorption of hydrogen and oxygen at elevated temperatures. (a) Section of the titanium tube that flattened as a result of test in accordance with ASTM B 337; the first crack was longitudinal
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