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symmetric laminates

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Published: 01 January 2001
Fig. 1 Local shear stress in a symmetric laminate subject to a uniform axial stress in the x -direction (σ x ). The global strain is shown, but there is no in-plane shear strain (γ xy ). Local shear stress (τ xy ) is developed in each ply. More
Image
Published: 01 January 2001
Fig. 2 Typical balanced-symmetric laminate More
Image
Published: 01 January 1997
Fig. 11 Symmetric laminate properties for carbon-fiber ( V F = 65%)/epoxy-resin composites with variable percentages of plies at 0, ±45, and 90°. (a) Tensile modulus. (b) Shear moudulus. (c) Poisson's ratio (tension). (d) A-basis tensile strength. (e) A-basis compression strength. (f More
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
... 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...
Image
Published: 01 January 1997
Fig. 12 Shape stability of right-angle laminates after cool-down from cure. All laminates are 90° before cure. (a) Symmetric laminate. The shrinkage in the matrix upon resin curing and the difference in coefficients of thermal expansion in-plane and through-plane cause a right angle to become More
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002478
EISBN: 978-1-62708-194-8
.... Composite laminates are constructed from lamina with uniaxial fiber orientation and frequently from textile fabrics as well. The article explains the characteristics of symmetric in-plane and through-thickness laminates; asymmetric in-plane and symmetric through-thickness laminates; asymmetric laminates...
Image
Published: 01 January 1997
Fig. 9 Deformation behavior of composites. The deformations for composites with various symmetries are schematically illustrated for in-plane loading and bending. Generally, laminates that are symmetric through the thickness and symmetric in-plane with respect to the applied stress are used More
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003385
EISBN: 978-1-62708-195-5
... for thin, symmetric, anisotropic plates. Orthotropic Plates In the full form of the plate equations, the terms D 16 and D 26 are bending-twisting coupling terms. If D 16 = D 26 = 0, then the plate is orthotropic in bending. Many composite laminates are not exactly orthotropic (see...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003398
EISBN: 978-1-62708-195-5
... in the “Glossary” in this Volume): Following are a list of common definitions relating to fibers and fabrics: The following terms apply to the resin used as a matrix as well as impregnating resins: Fig. 2 Typical balanced-symmetric laminate Fig. 3 Plain weave, yarn interlacing Fig...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003044
EISBN: 978-1-62708-200-6
..., and they will be discussed in more detail in the section on off-axis test specimens. Symmetric Laminates and Laminate Notation The principal material directions within each ply of a laminate are denoted by an x 1 - x 2 axis system. Laminate stacking sequences can be easily described for composites composed...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003387
EISBN: 978-1-62708-195-5
... (the z -direction in Fig. 1 ). Fig. 1 Local shear stress in a symmetric laminate subject to a uniform axial stress in the x -direction (σ x ). The global strain is shown, but there is no in-plane shear strain (γ xy ). Local shear stress (τ xy ) is developed in each ply...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003390
EISBN: 978-1-62708-195-5
... calculations. Lay-ups are entered in a tabular format, and special functions are available for creating symmetric laminates or rotating the entire laminate by some angle. These functions operate by simply copying plies, so it is not possible to undo a symmetry operation. Loads are entered as stresses...
Image
Published: 01 January 2000
Fig. 29 Schmatic of the laminate code (0/90/±45), for a composite material. The laminate code follows an ascending order from the bottom ply. The numerals are ply (or fiber) orientation with respect to the x-axis. The subscript s denotes that the laminate is symmetric with respect More
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003403
EISBN: 978-1-62708-195-5
... a good production tool. A carefully laid-up laminate, employing much attention to detail, will result in a high-quality mold or fixture that resists leaks and will perform for many cycles. As with other composite structures, it is recommended that a basic quasi-isotropic, balanced, and symmetrical...
Book Chapter

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
... ). All the plates discussed here are midplane symmetric, which eliminates bending-stretching coupling. It is, however, possible to include this effect in the analysis if asymmetrical laminates are used. The first ten modes of vibration of a typical plate can be adequately described by using a coarse...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003443
EISBN: 978-1-62708-195-5
... Abstract This article provides the general mechanical testing guidelines for the characterization of lamina and laminate properties. Guidelines are provided for tensile property, compressive property, shear property, flexure property, fracture toughness, and fatigue property test methods...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003046
EISBN: 978-1-62708-200-6
... to make a mold. The laminate stacking order was symmetric and continued to be even as internal plies were terminated. With this type of repair, locating the internal patch may require some ingenuity. With access limited to the external surface, the patch must be installed through the damage cutout...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003407
EISBN: 978-1-62708-195-5
... racers of 35 m or more, and large luxury cruising craft. The article discusses the tooling, laminating practice, curing, mold removal, and quality control, for manufacturing hulls, decks, masts, and appendages using composites. low-volume production sailing craft quality control composites...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003393
EISBN: 978-1-62708-195-5
... make the development of allowables significantly more difficult. Other design guidelines can further restrict the permissible design space, as is discussed later. Stacking sequence effects are important, however, even in a symmetric, balanced laminate. For failure modes influenced by bending loads...
Series: ASM Handbook
Volume: 21
Publisher: ASM International
Published: 01 January 2001
DOI: 10.31399/asm.hb.v21.a0003409
EISBN: 978-1-62708-195-5
.... Another complication for the glass fabric, wet lay- up technology was its inability to provide laminated components with tightly packed, accurately aligned fibers. The “runniness” of liquid wet lay-up resins cannot hold fibers where placed by laminator tools. To provide a stable material with combined...