Skip Nav Destination
Close Modal
By
David Arencón Osuna, Marcelo de Sousa Pais Antunes, Vera Cristina de Redondo Realinho, José Ignacio Velasco
Search Results for
strain energy release rate
Update search
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
NARROW
Format
Topics
Book Series
Date
Availability
1-20 of 487
Search Results for strain energy release rate
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
1
Sort by
Image
Published: 01 January 2001
Fig. 32 Strain energy release rate coefficients, C ε , for interfacial cracking in the 90°/90° and the–25°/ 90° interfaces of the [±25°/90°] s laminate
More
Image
Published: 01 January 2001
Fig. 33 Strain energy release rate coefficients, C T , for interfacial cracking in the 90°/90° and the–25°/ 90° interfaces of the [±25°/90°] s laminate
More
Image
Published: 01 January 2001
Fig. 37 Strain energy release rate coefficients, C ε , for transverse cracking in [0°/90° n /0°] laminates, n = 1, 2, 3, 4
More
Image
Published: 01 January 2001
Fig. 38 Strain energy release rate coefficients, C T , for transverse cracking in [0°/90° n /0°] laminates. n = 1, 2, 3, 4
More
Image
Published: 01 January 2001
Image
Published: 01 January 2001
Fig. 3 Critical strain energy release rate, G c , as a function of the mixed-mode ratio for graphite/epoxy IM7/E7T1-2. A, pure mode I; B, mixed mode I and mode II; C, pure mode II
More
Image
Published: 01 January 2000
Image
Published: 01 January 2001
Fig. 16 Local finite-element model of a damaged bondline used in strain energy release rate calculation for bonded joints. Source: Ref 29
More
Image
Published: 01 November 1995
Fig. 30 Plot of crack stability that is due to the R -curve of a material. Crack resistance, R , vs. extension is plotted on the same graph, along with applied strain-energy release rate, G . Catastrophic failure occurs at the stress when G = R c . After Ref 132
More
Image
Published: 01 January 2001
and a thicker, more stable sublaminate. (3) As the load increases, the thin sublaminate buckles and further out-of-plane loads result around the perimeter of the delamination. The postbuckling continues until the out-of-plane loads exceed the critical mode I strain energy release rate or the interlaminar
More
Image
in Effects of Composition, Processing, and Structure on Properties of Ceramics and Glasses
> Materials Selection and Design
Published: 01 January 1997
Fig. 14 Schematic representation of R -curve behavior. Crack resistance increases with crack length, so catastrophic failure will occur only when the strain energy release rate ( G ) exceeds the critical crack resistance value ( R c ). a o , initial crack size; a c , critical crack size
More
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003380
EISBN: 978-1-62708-195-5
... combination of fundamental modes to predict delamination onset and growth. Delamination Characterization Typical mixed-mode I and II delamination failure criterion is shown in Fig. 3 . The IFT is determined as a critical value of the strain energy release rate, G c , plotted as a function...
Abstract
Delamination is one of the most commonly observed failure modes in composite materials. This article describes the three fundamental fracture failure modes of composite delamination, namely, opening, in-plane shearing, and tearing or scissoring shearing modes. It discusses the characterization and analysis of delamination. The article also reviews the prediction of delamination factors, such as flexbeam fatigue life, and skin/stiffener pull-off strength and life.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003386
EISBN: 978-1-62708-195-5
... and further out-of-plane loads result around the perimeter of the delamination. The postbuckling continues until the out-of-plane loads exceed the critical mode I strain energy release rate or the interlaminar tension allowable. The final failure occurs as the delamination propagates perpendicular...
Abstract
This article addresses the issue of the implementation of composite damage tolerance requirements as it relates to military aircraft. It presents a brief introduction on the durability impact threat, damage tolerance impact threat, and other damage tolerance damage threats. The article summarizes damage tolerance criteria and durability criteria for military aircraft. It discusses the damage tolerance design philosophy for metallic structures and composite structures of the aircraft. The article describes the implementation of a damage tolerance analysis methodology in terms of the mechanics based model, the regression algorithm, and the semi-empirical analysis.
Book Chapter
Series: ASM Handbook
Volume: 11B
Publisher: ASM International
Published: 15 May 2022
DOI: 10.31399/asm.hb.v11B.a0006910
EISBN: 978-1-62708-395-9
..., such as plane-strain fracture toughness/strain energy release rate ( K Ic / G Ic ) methods, has been used for decades ( Ref 3 , 4 ). However, because of the inelasticity problems, polymers have stress distributions at the crack tip that cannot be described or quantified adequately by the assumptions...
Abstract
There are many different types of polymeric materials, ranging from glassy to semicrystalline polymers and even blends. Their mechanical properties range from pure elastic with very high strains to fracture (elastomers) to almost pure linear elastic (Hookian behavior) with low strains to fracture (glassy polymers). This article provides an overview of historical development of fracture behavior in polymers. It discusses the processes involved in three fracture test methods for polymers, namely linear elastic fracture mechanics, elastic-plastic fracture mechanics, and post-yield fracture mechanics.
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
... 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...
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.
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003310
EISBN: 978-1-62708-176-4
... to determine the plane strain fracture toughness of polymers. ASTM D 5045 specifies a procedure for determining the critical strain energy release rate, G Ic , of polymers. This parameter is equivalent to J Ic for materials that exhibit linear (or nearly linear) elastic behavior ( Ref 41 ). ASTM D 5045...
Abstract
This article discusses the J-integral-based single and multiple specimen techniques of the ASTM E 1737 test method for determining plane strain fracture toughness of polymeric materials. It describes the fracture toughness testing of thin sheets and films. The article concludes with information on the alternative methods for determining the fracture toughness of polymer materials.
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002379
EISBN: 978-1-62708-193-1
... postulated that the critical rate of strain energy released during unstable crack extension, G c , is related to the surface energy of the material, γ, as: (Eq 1) G c = 2 γ (Eq 2) G c = π σ c 2 a E where σ c is the critical stress at the onset of fracture and E...
Abstract
Fracture mechanics is a multidisciplinary engineering topic that has foundations in both mechanics and materials science. This article summarizes the microstructural aspect of fracture resistance in structural materials. It provides a discussion on basic fracture principles and schematically illustrates the mechanism of crack propagation. The article describes the fracture resistance of high-strength steels, aluminum alloys, titanium alloys, and composites such as brittle matrix-ductile phase composites and metal-matrix composites. It also lists the effects of microstructural variables on fracture toughness of steels, aluminum alloys, and titanium alloys.
Book: Composites
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003391
EISBN: 978-1-62708-195-5
... is developed and modeled separately. In the local model, boundary conditions are forced to match the deformations calculated by the global model at the edge of the patch. Using the fine mesh, local stresses, strains, interlaminar strain energy release rates, damage progression, and so forth can be calculated...
Abstract
Detailed analyses and test correlations are typically required to support design development, structural sizing, and certification. This article addresses issues concerning building block levels ranging from design-allowables coupons up through subcomponents, as these levels exhibit a wide variety of test-analysis correlation objectives. At these levels, enhanced analysis capability can be used most effectively in minimizing test complexity and cost while also reducing design weight and risk. The article discusses the examples of tests for which good correlative capability has shown significant benefit. These include notched (open and/or filled hole) tension and compression, inter/intralaminar shear and tension, and pin bearing.
Book Chapter
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003305
EISBN: 978-1-62708-176-4
... energy, U , is the work done by a load, P , causing a displacement, Δ: (Eq 7) U = P Δ / 2 = C P 2 / 2 where C = Δ/ P , the elastic compliance. The loss of elastic potential energy with crack extension of unit area, A , is defined as the strain-energy release rate...
Abstract
The fracture-mechanics technology has significantly improved the ability to design safe and reliable structures and identify and quantify the primary parameters that affect structural integrity of materials. This article provides a discussion on fracture toughness of notched materials by explaining the ductile-to-brittle fracture transition and by correlating KId, KIc, and Charpy V-notch impact energy absorptions. It highlights the effects of constraint, temperature, and loading rate on the fracture transition. The article discusses the applications of fracture mechanism in limiting of operating stresses. It describes the mechanisms, testing methods, and effecting parameters of two main categories of fracture mechanics: linear-elastic fracture mechanics and elastic-plastic fracture mechanics. The article concludes with a discussion on the three major progressive stages of fatigue: crack initiation, crack growth, and fracture on the final cycle.
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003330
EISBN: 978-1-62708-176-4
... energy release rate strain rate tension testing open hole tension test THE CHARACTERIZATION of engineering properties is a complex issue for fiber-reinforced composites (FRC) due to their inherent anisotropy and inhomogeneity. In terms of mechanical properties, advanced composite materials...
Abstract
This article begins with a review of the purposes of mechanical characterization tests and the general considerations related to the mechanical properties of anisotropic systems, specimen fabrication, equipment and fixturing, environmental conditioning, and analysis of test results. It provides information on the specimen preparation, instrumentation, and procedures for various mechanical test methods of fiber-reinforced composites. These include the compression test, flexure test, shear test, open hole tension test, and compression after impact test. The article describes three distinct fracture modes, namely, crack opening mode, shearing mode, and tearing mode. It presents an overview of fatigue testing and fatigue damage mechanisms of composite materials and reviews the types of mechanical measurements that can be made during the course of testing to assess fatigue damage. The article concludes with a discussion on the split-Hopkinson pressure bar test.
1