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Delamination Fracture In Graphite Epoxy Materials
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Book Synopsis Delamination Fracture in Graphite/Epoxy Materials by : Walter L. Bradley
Download or read book Delamination Fracture in Graphite/Epoxy Materials written by Walter L. Bradley and published by . This book was released on 1986 with total page 183 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Objectives; Summary Work Statement; Summary of Accomplishments by Areas in Work Statement: In-situ Fracture Observations, Crack tip Strain Field Measurements, Fracture Mechanics Characterization, Micromechanics Modeling, Fractography and Failure Analysis, Publications Resulting in Whole or in Part from Work Supported by AFOSR; Professional Personnel Associated with Research Effort; Presentations; Summary of Significance of Accomplishments; Papers: Micromechanics of Fracture in Toughened Graphite/Epoxy Laminates, A Comparison of the Crack Tip Damage Zone for Fracture of Hexcell F185 Neat Resin and T6C145/F185 Composite, The Relationship of Resin Ductility and Composite Delamination, Delamination Analysis of Composites with Distributed Damage using a J integral, Correlation Between Micromechanical Failure Processes and the Delamination Fracture Toughness of Graphite/Epoxy Composite, The Meaning and Significance of Hackles in Composite Materials Failure Analysis.
Book Synopsis Hygrothermal Influence on Delamination Behavior of Graphite/epoxy Laminates by :
Download or read book Hygrothermal Influence on Delamination Behavior of Graphite/epoxy Laminates written by and published by . This book was released on 1984 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effect of Resin Toughness on the Delamination Fracture Behavior of Graphite/epoxy Composites by : William Mark Jordan
Download or read book The Effect of Resin Toughness on the Delamination Fracture Behavior of Graphite/epoxy Composites written by William Mark Jordan and published by . This book was released on 1985 with total page 412 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Delamination and Debonding of Materials by : W. Steven Johnson
Download or read book Delamination and Debonding of Materials written by W. Steven Johnson and published by ASTM International. This book was released on 1985 with total page 507 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Mode II Delamination Fracture Toughness of Unidirectional Graphite/Epoxy Composites by : WL. Bradley
Download or read book Mode II Delamination Fracture Toughness of Unidirectional Graphite/Epoxy Composites written by WL. Bradley and published by . This book was released on 1989 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt: The mode II delamination fracture toughness of a ductile and a brittle unidirectional graphite/epoxy composite has been studied using the end-notched flexure (ENF) test and the end-loaded split laminate (ELS) test. The stress field in the vicinity of the crack tip of a split laminate beam under mode I and mode II (ELS test) conditions has been determined by means of a finite-element analysis. Also, the micromechanics of mode II fracture have been studied during in situ and postmortem observations of the fracture process. Both the ENF and ELS tests give similar values for GIIc. However, because elastic material behavior is assumed in the analysis, the GIIc results for a ductile composite are somewhat uncertain because permanent deformation is observed. The ELS test provides a pure shear stress state in the vicinity of the crack tip. The formation of hackles in composites made with brittle resins provides a more tortuous path for the crack leading to an increased resistance to delamination under mode II conditions compared to mode I. However, extensive resin deformation and yielding play a more significant role in the fracture resistance for mode II loading of composites made using a rubber-toughened epoxy.
Book Synopsis Load Rate Effects on Delamination Fracture Toughness of Graphite/epoxy Composites by : James Wayne Auser
Download or read book Load Rate Effects on Delamination Fracture Toughness of Graphite/epoxy Composites written by James Wayne Auser and published by . This book was released on 1985 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Delamination Fracture Toughness and Acoustic Emission in Fiber-reinforced Epoxy Laminates by : Hamid Saghizadeh
Download or read book Delamination Fracture Toughness and Acoustic Emission in Fiber-reinforced Epoxy Laminates written by Hamid Saghizadeh and published by . This book was released on 1987 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Delamination Fracture Toughness of a Unidirectional Graphite/epoxy Composite by : Roy Charles Hulsey
Download or read book Delamination Fracture Toughness of a Unidirectional Graphite/epoxy Composite written by Roy Charles Hulsey and published by . This book was released on 1980 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Mode II Delamination Fracture Toughness of Unidirectional Graphite/epoxy Composites by : Carlos Roberto Corleto Mena
Download or read book Mode II Delamination Fracture Toughness of Unidirectional Graphite/epoxy Composites written by Carlos Roberto Corleto Mena and published by . This book was released on 1986 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Delamination Buckling of Composite Materials by : L. Kachanov
Download or read book Delamination Buckling of Composite Materials written by L. Kachanov and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 101 pages. Available in PDF, EPUB and Kindle. Book excerpt: LIOn Delamination of Laminated Composites (a) Fiber-Reinforced Composites Considerable technological advances in the production of high-strength fibers (graphite, boron, etc.) have led to a wide use of light high-strength composite materials (graphite epoxy, boron-epoxy, etc.). It is expedient, to make thin walled composite rods, plates, and shells from such materials. Plates can be made by bonding a set of unidirectional thin fiber layers, Fig.l.l. Such plates are orthotropic, as a rule. A random short-fiber composite is shown in Fig. 1.2. Fiber-reinforced composites are widely used in thin-walled aircraft structures because of their specific high strength. For example, the graphite-epoxy composite is characterized by a unidirectional tensile strength of 1.4 GPa while the density is 1.6 Mg/rrt? . For comparison, we may take a steel (steel 4340) whose corresponding properties are identified by values like 1.2 GPa and 7.8 Mg/rrt? . 1. INTRODUCTION Figure 1.1 2 1.1. On Delamination of Laminated Composites Figure 1.2 3 1. INTRODUCTION It is characteristic for laminated plastic material to possess a fairly low bonding. Therefore, low-velocity impacts and defects in manufacturing lead to local delamination. (b) Linear Problems of Delamination Buckling Delamination can significantly reduce the compressive strength and stiffness of the laminate. Local delamination can be considered as a crack in the bond. Under buckling there appears a high interlaminate stress at the crack edge that leads to a spreading of the crack. Delamination growth can lead to structural instability.
Book Synopsis Rate Effects on Delamination Fracture Toughness of a Toughened Graphite/Epoxy by : AA. Aliyu
Download or read book Rate Effects on Delamination Fracture Toughness of a Toughened Graphite/Epoxy written by AA. Aliyu and published by . This book was released on 1987 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of this study was to determine the effects of loading rate on interlaminar fracture toughness of T300/F-185 graphite/epoxy composite, having an elastomer-modified epoxy resin matrix. Mode I interlaminar fracture was investigated by means of uniform width and width-tapered double cantilever beam (DCB) specimens. Hinged tabs were used to insure unrestrained rotation at the free ends. Specimens were loaded at quasi-static deflection rates of up to 8.5 mm/s (20 in./min) corresponding to crack extension rates of up to 21 mm/s (49.6 in./min). Crack extension was monitored by means of strain gages mounted on the surface of the specimen. Continuous records were obtained of load, deflection, and crack extension for determination of the strain energy release rate. The latter was calculated by means of the area method and beam analysis method, and expressed as a power law of the crack extension velocity. Results indicate that the strain energy release rate decreases with crack velocity by over 20% over three decades of crack velocity.
Book Synopsis Moisture and Temperature Effects on the Mixed-Mode Delamination Fracture of Unidirectional Graphite/Epoxy by : AJ. Russell
Download or read book Moisture and Temperature Effects on the Mixed-Mode Delamination Fracture of Unidirectional Graphite/Epoxy written by AJ. Russell and published by . This book was released on 1985 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: The critical strain energy release rates for interlaminar fracture of unidirectional graphite/epoxy, both from a sharp notch and as a function of crack extension, were determined experimentally for combined tensile/shear loadings. Based on well-founded compliance techniques, a substantial database was generated over the temperature range -50°C to 100°C for both dry and moisture-saturated states. The fracture energy of the unreinforced epoxy matrix material was also measured. Initiation energies for delamination increased as the proportion of shear loading increased and as the temperature was lowered but were insensitive to moisture content. The fracture resistance to crack extension increased under tensile dominated loadings with both temperature and moisture content but remained constant for high shear loadings. The applicability of various mixed-mode fracture criteria to both the present data and to available literature data is examined. The Wu fracture model was modified to take into account plane strain conditions appropriate to delamination. Crack growth resistance behavior is discussed in terms of the micromechanisms occurring close to the crack tip.
Book Synopsis Fracture Mechanics of Matrix Cracking and Delamination in Glass/epoxy Laminates by : M. Caslini
Download or read book Fracture Mechanics of Matrix Cracking and Delamination in Glass/epoxy Laminates written by M. Caslini and published by . This book was released on 1986 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study focused on characterizing matrix cracking and delamination behavior in multidirectional laminates. Static tension and tension-tension fatigue tests were conducted on two different layups. Damage onset, accumulation, and residual properties were measured. Matrix cracking was shown to have a considerable influence on residual stiffness of glass epoxy laminates, and could be predicted reasonably well for cracks in 90 deg plies using a simple shear lag analysis. A fracture mechanics analysis for the strain energy release rate associated with 90 deg ply matrix crack formation was developed and was shown to correlate the onset of 90 deg ply cracks in different laminates. The linear degradation of laminate modulus with delamination area, previously observed for graphite epoxy laminates, was predicted for glass epoxy laminates using a simple rule of mixtures analysis. The strain energy release rate associated with edge delamination formation under static and cyclic loading was difficult to analyze because of the presence of several contemporary damage phenomena. Keywords: Fatigue(Mechanics), and Stiffness loss.
Book Synopsis Mode I - Mode II Delamination Fracture Toughness of a Unidirectional Graphite/epoxy Composite by : Peter Stephen Vanderkley
Download or read book Mode I - Mode II Delamination Fracture Toughness of a Unidirectional Graphite/epoxy Composite written by Peter Stephen Vanderkley and published by . This book was released on 1981 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Dynamic Delamination Crack Propagation in a Graphite/epoxy Laminate by :
Download or read book Dynamic Delamination Crack Propagation in a Graphite/epoxy Laminate written by and published by . This book was released on 1991 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Composite Materials by : Samuel P. Garbo
Download or read book Composite Materials written by Samuel P. Garbo and published by ASTM International. This book was released on 1990 with total page 589 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation Papers from the symposium held April 1988 in Sparks, Nevada. The focus is on significant advances in the area of damage tolerance and durability of composite structures. Twenty-seven contributions address delamination initiation and growth analysis, damage mechanisms and test procedures, and other general interest design and analysis topics. Annotation copyrighted by Book News, Inc., Portland, OR.
Book Synopsis Effects of Strain Rate on Delamination Fracture Toughness of Graphite/Epoxy by : AA. Aliyu
Download or read book Effects of Strain Rate on Delamination Fracture Toughness of Graphite/Epoxy written by AA. Aliyu and published by . This book was released on 1985 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of this paper is to evaluate various experimental techniques and analysis methods for the characterization of interlaminar fracture toughness, and to determine the effects of strain rate on that property for a graphite/epoxy composite. Mode I interlaminar fracture was investigated by means of a double-cantilever beam (DCB) specimen for AS-4/3501-6 graphite/epoxy. Hinged tabs were used to insure unrestrained rotation at the free ends. Specimens were loaded at quasi-static deflection rates of up to 8.5 mm/s (20 in./min) corresponding to crack extension rates of over 51 mm/s (2 in./s). Crack extension was monitored by means of strain gages mounted on the surface of the specimen, or a conductive-paint circuit attached to the edge of the DCB specimen. Continuous records were obtained of load, deflection, and crack extension for determination of the strain energy release rate. The latter was expressed as a power law of the crack extension velocity. Results indicate that the strain energy release rate increases with crack velocity by up to 28% for the range of rates considered here.