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Book Chapter
Mechanical Behavior Under Tensile and Compressive Loads
Available to PurchaseSeries: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003261
EISBN: 978-1-62708-176-4
.... The point of necking at maximum load can be obtained from the true stress-true strain curve by finding the point on the curve having a subtangent of unity. The article concludes with an overview of the ductility measurements performed by notch tensile and compression tests. mechanical behavior...
Abstract
This article focuses on mechanical behavior of materials under conditions of uniaxial tension and compression. The emphasis is on mechanical behavior during the engineering tension test, which is used to provide basic design information on the strength of materials and as an acceptance test for the specification of materials. The article presents mathematical expressions for a flow curve of many metals in the region of uniform plastic deformation. It explains that the rate at which strain is applied to the tension specimen has an important influence on the stress-strain curve. The point of necking at maximum load can be obtained from the true stress-true strain curve by finding the point on the curve having a subtangent of unity. The article concludes with an overview of the ductility measurements performed by notch tensile and compression tests.
Image
Crack-initiation locations in compression loading. Crack initiation may occ...
Available to Purchase
in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 89 Crack-initiation locations in compression loading. Crack initiation may occur along the centerline and at the surface on a hoop plane. Further deformation may close the centerline crack.
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Image
Crack-initiation locations in compression loading. Crack initiation can occ...
Available to Purchase
in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 89 Crack-initiation locations in compression loading. Crack initiation can occur along the centerline and at the surface on a hoop plane. Further deformation can close the centerline crack.
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Image
Shear test fixture of the compression loading type used for single or doubl...
Available to PurchasePublished: 01 December 1998
Fig. 51 Shear test fixture of the compression loading type used for single or double shear test. Courtesy Tinius Olsen Testing Machine Company
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Image
Compressive deformation versus the biaxial shear-compression load ratio for...
Available to PurchasePublished: 01 January 2000
Fig. 20 Compressive deformation versus the biaxial shear-compression load ratio for titanium alloy Ti-6Al-4V and several tungsten alloys (see text). Open symbols: uniform deformation, no cracks, no failures; symbols with a cross inside: first tensile or shear cracks, (normal) shear failure
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Image
Ratio of shear load to compressive load as a function of specimen inclinati...
Available to PurchasePublished: 01 January 2000
Fig. 15 Ratio of shear load to compressive load as a function of specimen inclination to the loading axis
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Image
Extrapolation method to correct for end effects in compressive loading. Sou...
Available to PurchasePublished: 01 January 2005
Image
Extrapolation method to correct for end effects in compressive loading. Sou...
Available to PurchasePublished: 01 January 2005
Image
Deformability behavior under pure compressive loading as function of strain...
Available to PurchasePublished: 01 January 2000
Fig. 18 Deformability behavior under pure compressive loading as function of strain rate for titanium alloy Ti-62222Si. Open circles, failure under stable plastic flow; solid circles, failure with adiabatic shear bands
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Image
Shear stresses produced by a cylindrical roller under compressive load belo...
Available to Purchase
in Failures of Rolling-Element Bearings and Their Prevention
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 46 Shear stresses produced by a cylindrical roller under compressive load below the surface of the bearing raceway. Adapted from Ref 42
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Book: Composites
Series: ASM Handbook Archive
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003382
EISBN: 978-1-62708-195-5
... Abstract In the design of composite structures for durability and damage tolerance, the primary concerns are out-of-plane failures, such as delamination, material degradation associated with environment, stability under compression loading, large degree of scatter in fatigue life, and bearing...
Abstract
In the design of composite structures for durability and damage tolerance, the primary concerns are out-of-plane failures, such as delamination, material degradation associated with environment, stability under compression loading, large degree of scatter in fatigue life, and bearing failure of joints. This article presents an introductory discussion on the fatigue damage process, methodologies assessing fatigue behavior, and life prediction models. It describes the damage mechanisms introduced for a quasi-isotropic laminate under tension-compression fatigue loading. Delamination is a critical issue in fatigue and generally results from high interlaminar normal and shear stresses. The article schematically illustrates the structural elements in which high interlaminar stresses are common. It concludes with a discussion on the classification of fatigue models such as mechanistic or phenomenological, for composite materials under cyclic loading.
Book: Fractography
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 June 2024
DOI: 10.31399/asm.hb.v12.a0006845
EISBN: 978-1-62708-387-4
..., tension, bending, and compressive loads. This article discusses tools and techniques of visual examination and characteristic features of fracture features. A brief review of ductile and brittle fracture-surface features is provided. The article also describes macroscopic features that can be used...
Abstract
Fracture surfaces can provide an important and indispensable record of many factors in simple or complex failures. Visual examination of fracture surfaces can reveal the type and direction of loading, with fracture-surface features often providing definitive evidence of torsion, tension, bending, and compressive loads. This article discusses tools and techniques of visual examination and characteristic features of fracture features. A brief review of ductile and brittle fracture-surface features is provided. The article also describes macroscopic features that can be used to identify fracture-initiation sites, locations of final overload, and the directions of crack propagation. In addition, the use of these features to characterize loading at the time of failure is also described.
Book Chapter
Fatigue of Brittle Materials
Available to PurchaseBook: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002417
EISBN: 978-1-62708-193-1
... ceramics, and ceramic composites under cyclic compression. The cyclic damage zones ahead of tensile fatigue cracks, crack propagation under cyclic tension or tension-compression loads, and elevated-temperature fatigue crack growth in monotonic and composite ceramics, are discussed. The article presents...
Abstract
This article summarizes the understanding of the mechanisms and mechanical effects of fatigue processes in highly brittle materials, with particular emphasis on ceramics. It provides a discussion on room-temperature fatigue crack growth in monolithic ceramics, transformation-toughened ceramics, and ceramic composites under cyclic compression. The cyclic damage zones ahead of tensile fatigue cracks, crack propagation under cyclic tension or tension-compression loads, and elevated-temperature fatigue crack growth in monotonic and composite ceramics, are discussed. The article presents ceramic fatigue data for fatigue crack growth testing and concludes with a discussion on life prediction for ceramics or ceramic-matrix composites.
Image
Schematic of the modified maneuver spectrum and a detail showing five compr...
Available to PurchasePublished: 01 June 2024
Fig. 15 Schematic of the modified maneuver spectrum and a detail showing five compressive loads that resulted in marker bands. These compressive loads were inserted between several high loads approximately halfway through the spectrum.
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Image
Generic types of compression test methods. (a) Shear loaded. (b) End-loaded...
Available to PurchasePublished: 01 January 2000
Fig. 9 Generic types of compression test methods. (a) Shear loaded. (b) End-loaded. (c) Sandwich beam specimen.
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Image
Example of the Bauschinger effect and hysteresis loop in tension-compressio...
Available to PurchasePublished: 01 January 2000
Fig. 6 Example of the Bauschinger effect and hysteresis loop in tension-compression-tension loading. This example shows initial tension loading to 1% strain, followed by compression loading to 1% strain, and then a second tension loading to 1% strain.
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Estimation of the bivariate size-orientation distribution function of micro...
Available to Purchase
in Quantitative Characterization and Representation of Global Microstructural Geometry
> Metallography and Microstructures
Published: 01 December 2004
compressive stress deformed to 0.7 strain. (b) The estimated 3-D bivariate size and orientation distribution of the microcracks. All angles are measured with respect to the loading direction (vertical axis). In compression, the majority of the microcracks are parallel to the direction of applied compressive
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Image
A curved laminate “C” channel in various loading conditions. (a) Unloaded. ...
Available to PurchasePublished: 01 January 2001
Fig. 4 A curved laminate “C” channel in various loading conditions. (a) Unloaded. (b) Radii open under tensile load. (c) Radii close under compressive load
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Image
The orientation of the actual weld throat provides evidence of the principa...
Available to Purchase
in Failure Analysis of Welded Structures
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Image
(a) Unloaded condition of a fillet weld with slight gap in root. (b) Gap re...
Available to Purchase
in Failure Analysis of Welded Structures
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 11 (a) Unloaded condition of a fillet weld with slight gap in root. (b) Gap reduced resulting in bearing due to static compression. (c) Possible cracking due to cyclic compressive loads.
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