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Published: 01 November 2010
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Published: 01 November 2010
Book Chapter
Composite Structure Analysis
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030137
EISBN: 978-1-62708-349-2
... in manufacturing the part. Although this can be the case, and is most often used for modeling purposes, the manufacturing process/cure cycle adds another variable that dictates the final performance. While through-thickness uniformity is usually assumed, fiber volume variations, void content, ply orientation...
Abstract
Analyzing the structure of composite materials is essential for understanding how the part will perform in service. Assessing fiber volume variations, void content, ply orientation variability, and foreign object inclusions helps in preventing degradation of composite performance. This chapter describes the optical microscopy and bright-field illumination techniques involved in analyzing ply terminations, prepreg plies, splices, and fiber orientation to provide the insight necessary for optimizing composite structure and performance.
Book Chapter
Pressure Vessel Design, Fabrication, Analysis, and Testing
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 September 2011
DOI: 10.31399/asm.tb.cfw.t52860115
EISBN: 978-1-62708-338-6
... diagram for a pressure vessel is shown in Fig. 9.4 . Summing the running loads in the longitudinal direction, N φ , the following relationships are obtained. Fig. 9.4 Netting analysis free-body diagram For the purpose of this discussion, a typical ply thickness, T , for most applications...
Abstract
The necessity of developing the lightest-weight structures with sufficient strength was the driving factor for the development of filament-wound composite pressure vessels. This chapter presents a brief history of the development of rocket motor cases (RMCs), followed by a comparison of the advantages of composites over metals for RMCs. A discussion on a typical design, analysis, and manufacturing operation follows. The chapter introduces the basic design approach and shows some sizing techniques along with example calculations. It discusses the processes involved in the testing of the composite pressure vessel.
Book Chapter
Processing Science of Polymer Matrix Composites
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870201
EISBN: 978-1-62708-314-0
... because (1) thick laminates usually drive thick tools that exhibit very slow heat-up rates and (2) thick laminate parts are often made in matched metal tools. In order to get the lay-up to fit within these tools, the plies, or ply packs, either have to be hot debulked if the material is a net resin...
Abstract
This chapter provides an overview of the tools and techniques, as well as some of the underlying theory, that have proven useful for process modeling and simulation. It begins by presenting the framework of a thermoset cure model that accounts for kinetics, viscosity, heat transfer, flow, voids, and residual stress. It then discusses each variable in detail, explaining how it affects the cure process, how it is measured, and how it can be expressed mathematically in the form of a simple model. The discussions throughout the chapter are supported by numerous images, diagrams, and data plots.
Book Chapter
Fibers and Reinforcements
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870031
EISBN: 978-1-62708-314-0
.... Twisting improves the handleability and makes processes such as weaving easier, but the twist also reduces the strength properties. Band —The thickness or width of several rovings, yarns, or tows as it is applied to a mandrel or tool; a common term used in filament winding. Tape —A composite...
Abstract
This chapter discusses the properties and processing characteristics of glass, aramid, carbon, and ultra-high molecular weight polyethylene fibers and related product forms, including woven fabrics, prepreg, and reinforced mats. It also includes a review of fiber terminology as well as physical and mechanical property data for commercially important high-strength fibers.
Book Chapter
Thermoplastic Composite Fabrication Processes
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870183
EISBN: 978-1-62708-314-0
... The primary preheating methods used for press thermoforming are IR heater banks, convection ovens, and heated platen presses. In IR heating the heating time is typically short, in this case, one to two minutes, but temperature gradients can form within thick ply packs. Since the surface heats considerably...
Abstract
This chapter discusses thermoplastic composite fabrication processes and related equipment and procedures. The discussion covers consolidation and thermoforming operations as well as joining methods.
Book Chapter
Structural Analysis
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870421
EISBN: 978-1-62708-314-0
... of the plies are oriented in the zero-degree or 90-degree direction. An example is the four-ply thick zero-degree laminate [0°, 0°, 0°, 0°]. Note that this is the same as a single ply or lamina, only thicker, as a result of multiple layers. Angle-Ply Laminates In an angle-ply laminate, all of the plies...
Abstract
This chapter discusses some of the challenges associated with the analysis of composite structures. It begins with a review of lamina fundamentals and the stress-strain relationships in a single ply under various types of loads. It demonstrates the use of classical lamination theory, discusses the effects of interlaminar free-edge stresses, and explains how to predict the failure of composites using stress and strain criteria as well as the Azzi-Tsai-Hill maximum work theory and the Tsai-Wu failure criterion.
Book Chapter
Microcrack Analysis of Composite Materials
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030159
EISBN: 978-1-62708-349-2
.... The interlayer thickness and modulus, ply orientations, thickness of the ply layers, and the grouping of the plies affect the stress/strain levels at which microcracking occurs in fiber-rein-forced composites ( Ref 6 to 9 ). The residual stresses in a composite material act to preload the composite and can...
Abstract
The formation of microcracks in composite materials may arise from static-, dynamic-, impact-, or fatigue-loading situations and also by temperature changes or thermal cycles. This chapter discusses the processes involved in the various methods for the microcrack analysis of composite materials, namely bright-field analysis, polarized-light analysis, contrast dyes analysis, and dark-field analysis. The analysis of microcracked composites using epi-fluorescence is also covered. In addition, the chapter describes the procedures for the determination and recording of microcracks in composite materials.
Book Chapter
Design and Certification Considerations
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870489
EISBN: 978-1-62708-314-0
... fiber wet-out, structural efficiency (minimize ply thickness), surface finish 12K tow 3K tow Fiber modulus (if carbon is selected) Cost stiffness, weight, brittleness Lowest-modulus carbon Highest-modulus carbon Fiber form (continuous vs. discontinuous) Cost, strength, stiffness, weight...
Abstract
This chapter discusses design and certification considerations, including materials and process selection, the building block approach to certification, design allowables, and design guidelines. It also includes information on damage tolerance and environmental sensitivity.
Book Chapter
Mechanics of Fiber-Reinforced Composites
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540319
EISBN: 978-1-62708-309-6
...) A ¯ i j = Σ i − 1 k ( Q ¯ i j ) i ( z i − z i − 1 ) / B Here ( Z i − Z i –1 ) is the thickness of the i th ply, and B is the total thickness of the laminate. The bar denoting average has been dropped and the stresses...
Abstract
This chapter discusses the failure mechanisms associated with fiber-reinforced composites. It begins with a review of fiber-matrix systems and the stress-strain response of unidirectional lamina and both notched and unnotched composite laminate specimens. It then explains how cyclic loading can lead to delamination, the primary failure mode of most composites, and describes some of the methods that have been developed to improve delamination resistance, assess damage tolerance, determine residual strength, and predict failure modes.
Book Chapter
Tensile Testing of Fiber-Reinforced Composites
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.tt2.t51060183
EISBN: 978-1-62708-355-3
... of the same material with equal ply thickness by simply listing the ply orientations from the top of the laminate to the bottom. Thus, the notation [0°/90°/0°] uniquely defines a three-layer laminate. The angle denotes the orientation of the principal material axis, x 1 , within each ply. If a ply were...
Abstract
This chapter presents the fundamentals of tensile testing of fiber-reinforced polymer composites. Basic tensile testing of polymer composites is divided into lamina and laminate testing. The chapter focuses on tensile testing of laminates. It discusses the most common tensile test methods that have been standardized for fiber-reinforced composite materials. It also briefly reviews considerations in tensile testing of metal-matrix composites.
Book Chapter
Void Analysis of Composite Materials
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030147
EISBN: 978-1-62708-349-2
... in the low-pressure areas. Likewise, tubular composite parts that have thick cross sections and high ply angles can cause large constraints during the compaction process that can resist even the highest applied pressures. Accordingly, these types of composites may contain more voids. This is often found...
Abstract
Achieving the best-performing composite part requires that the processing method and cure cycle create high-quality, low-void-content structures. If voids are present, the performance of the composite will be significantly reduced. There are multiple causes of voids in composite materials; they are generally categorized as voids that are due to volatiles (such as solvents, water) or voids that result from entrapped air. This chapter describes the analysis of various types of voids. It reviews techniques for analysis of voids at ply-drops, voids due to high fiber packing, and voids that occur in honeycomb core composites. The final section of the chapter discusses void documentation through the use of nondestructive inspection techniques and density/specific gravity measurement methods.
Image
Composite cross section showing many of the different facets that are usual...
Available to Purchase
in Viewing the Specimen Using Reflected-Light Microscopy
> Optical Microscopy of Fiber-Reinforced Composites
Published: 01 November 2010
Fig. 5.2 Composite cross section showing many of the different facets that are usually investigated using reflected-light bright-field illumination. Shown in the cross section are voids (dark areas), ply terminations (i.e., ply drops), carbon fiber plies having different thicknesses, different
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Book Chapter
Fatigue and Fracture of Continuous-Fiber Polymer-Matrix Composites
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2012
DOI: 10.31399/asm.tb.ffub.t53610377
EISBN: 978-1-62708-303-4
...° plies. Matrix cracking in a [0°/90°/±45°] s laminate is shown in Fig. 18 . More and more matrix cracks develop until they reach a steady-state or saturation level that is a function of ply thickness and material properties. The damage during this phase is relatively small and occurs during the first...
Abstract
Unlike metals, in which fatigue failures are due to a single crack that grows to a critical length, the effects of fatigue in composites are much more distributed and varied. As the chapter explains, there are five major damage mechanisms that contribute to the progression of composite fatigue, those being matrix cracking, fiber breaking, crack coupling, delamination initiation, and delamination growth. The chapter describes each mechanism in detail along with related factors. It also discusses the primary differences between composites and metals, the effect of manufacturing defects, damage tolerance, and testing and certification.
Image
Schematic showing the sectioning of a composite part on an angle through th...
Available to PurchasePublished: 01 November 2010
Fig. 7.9 Schematic showing the sectioning of a composite part on an angle through the thickness. This is done to elongate the fibers for easier determination of the ply angles.
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Book Chapter
Thermoset Composite Fabrication Processes
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870119
EISBN: 978-1-62708-314-0
... of manually collating the laminate in the flat condition and then using a vacuum bag to form it to the contour of the tool. If the laminate is thick, this process may have to be done in several steps to prevent wrinkling and buckling of the ply packs. Heat (<150 °F (65 °C)) can be used to soften the resin...
Abstract
This chapter familiarizes readers with the many and varied thermoset composite fabrication processes and the types of applications for which they were developed. It describes wet lay-up, prepreg lay-up, and low-temperature vacuum bag curing prepreg processes, which are best suited for low-volume, medium-sized and larger parts. It also discusses filament winding and preforming processes (including weaving, knitting, stitching, and braiding) in addition to resin-transfer molding, resin film infusion, and pultrusion.
Image
Coordinates defined for composite material sample preparation as related to...
Available to PurchasePublished: 01 November 2010
Fig. 2.1 Coordinates defined for composite material sample preparation as related to sectioning and viewing planes. Sectioning through the composite thickness on an angle helps in determining ply orientations (i.e., fibers will become elongated).
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Book
Series: ASM Technical Books
Publisher: ASM International
Published: 01 September 2011
DOI: 10.31399/asm.tb.cfw.9781627083386
EISBN: 978-1-62708-338-6
Book Chapter
Static Mechanical Tests for Filament-Wound Composites
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 September 2011
DOI: 10.31399/asm.tb.cfw.t52860095
EISBN: 978-1-62708-338-6
... Method for Transverse Tensile Properties of Hoop-Wound Polymer-Matrix Composite Cylinders ASTM D 7291/D 7291M-07 Standard Test Method for Through-Thickness “Flatwise” Tensile Strength and Elastic Modulus of a Fiber-Reinforced Polymer-Matrix Composite Material Some ASTM standards for composite...
Abstract
The objective of mechanical testing of an engineered material is to provide data necessary for the analysis, design, and fabrication of structural components using the material. The testing of filament-wound composite materials offers unique challenges because of the special characteristics of composites. This chapter describes suitable static mechanical test techniques for characterizing laminated composite materials. The approach is to provide recommended techniques, based on consensus opinions of fabricators and users of filament-wound composites, and to survey available techniques that have been used successfully in the field. The chapter describes the effects of various factors on the properties of composite constituents, including fibers, resins, and unidirectional plies. Some aspects of specimen selection are also described. The chapter provides information on pressure bottles and tubular parts that have been developed as standard test specimens for combined load testing of composites.
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