Type of site | Cloud computing |
---|---|
Available in | English, Spanish, Portuguese, Persian |
Headquarters | Morgantown, West Virginia |
Created by | Ever J. Barbero |
URL | cadec-online |
Registration | Required |
Launched | February 9, 2011 |
Current status | Inactive |
Content licence | Terms and Conditions |
Written in | ASP.NET, C#, Fortran |
cadec-online.com was a multilingual web application that performs analysis of composite materials [1] and is used primarily for teaching, [2] especially within the disciplines of aerospace engineering, materials science, naval engineering, [3] mechanical engineering, [4] and civil engineering. Users navigate the application through a tree view which structures the component chapters. cadec-online is an engineering cloud application. [5] It uses the LaTeX library to render equations and symbols, then Sprites to optimize the delivery of images to the page. As of 2021, the application is no longer available.
cadec-online.com implements micromechanics for composites reinforced with unidirectional fibers, and random fibers, as well as plain weave, twill, and satin textiles. It predicts lamina elastic moduli, strength values, coefficient of thermal expansion (CTE), moisture expansion, and other micromechanical properties. The application conducts this analysis through several theoretical models, including:
cadec-online.com can calculate the three-dimensional (3D) stiffness and compliance matrices, the two-dimensional (2D) reduced stiffness and compliance matrices, in lamina coordinate system (cs). It is also capable of transforming the composite laminates matrices to any other coordinate system. Lamina types supported by the software include:
The application can carry out laminate analyses including calculation of laminate stiffness, stress, strain, and failure. The software supports intact and damaged laminates (see damage mechanics). For each category, cadec-online.com can calculate the laminate thermal stresses, laminate coefficient of thermal expansion, laminate stiffness and compliance matrices for composite laminates. Also, the application can predict the laminate moduli, which are orthotropic material equivalents for the stiffness of the laminate in both bending and membrane modes of deformation.
cadec-online.com predicts failures such as first ply failure (FPF) and last ply failure (LPF) under mechanical, thermal, and moisture loads, as well as in situ effects, using several failure criteria (FC) including:
Uses discrete damage mechanics (DDM) to predict crack density vs. strain for any symmetric laminate subjected to any membrane state of strain. The results can be exported to Excel for plotting. The state variable describing the damage state of the material is the crack density in each ply. The thermodynamic force is the midsurface strain applied to the laminate. The relevant material properties are the fracture toughnesses in modes I (opening) and II (shear) of the ply.
The application can predict the stiffness and strength of composite materials reinforced with plain weave, twill, and satin textile, also called fabric. The textile lamina is idealized as a transversely isotropic material. The calculated textile lamina can be used as any other lamina in the rest of the application. The calculated properties include:
The application is able to analyze laminated composite thin walled beams with general cross sections. Beams can be asymmetric and loaded by general combinations of forces in three planes (axial, vertical and horizontal) as well as by three moments (torque and two bending moments). cadec-online.com computes section properties such as the shear center.
cadec-online.com defines four different types of loads:
cadec-online.com features an API that allows users to access virtually all of the capabilities present in the web version of the software from other software environments such as Abaqus, Ansys, Matlab, Python, .NET Framework, Mathematica, etc. [13]
In materials science, a metal matrix composite (MMC) is a composite material with fibers or particles dispersed in a metallic matrix, such as copper, aluminum, or steel. The secondary phase is typically a ceramic or another metal. They are typically classified according to the type of reinforcement: short discontinuous fibers (whiskers), continuous fibers, or particulates. There is some overlap between MMCs and cermets, with the latter typically consisting of less than 20% metal by volume. When at least three materials are present, it is called a hybrid composite. MMCs can have much higher strength-to-weight ratios, stiffness, and ductility than traditional materials, so they are often used in demanding applications. MMCs typically have lower thermal and electrical conductivity and poor resistance to radiation, limiting their use in the very harshest environments.
A composite material is a material which is produced from two or more constituent materials. These constituent materials have notably dissimilar chemical or physical properties and are merged to create a material with properties unlike the individual elements. Within the finished structure, the individual elements remain separate and distinct, distinguishing composites from mixtures and solid solutions.
Young's modulus is a mechanical property of solid materials that measures the tensile or compressive stiffness when the force is applied lengthwise. It is the modulus of elasticity for tension or axial compression. Young's modulus is defined as the ratio of the stress applied to the object and the resulting axial strain in the linear elastic region of the material.
Engineered wood, also called mass timber, composite wood, human-made wood, or manufactured board, includes a range of derivative wood products which are manufactured by binding or fixing the strands, particles, fibres, or veneers or boards of wood, together with adhesives, or other methods of fixation to form composite material. The panels vary in size but can range upwards of 64 by 8 feet and in the case of cross-laminated timber (CLT) can be of any thickness from a few inches to 16 inches (410 mm) or more. These products are engineered to precise design specifications, which are tested to meet national or international standards and provide uniformity and predictability in their structural performance. Engineered wood products are used in a variety of applications, from home construction to commercial buildings to industrial products. The products can be used for joists and beams that replace steel in many building projects. The term mass timber describes a group of building materials that can replace concrete assemblies.
The field of strength of materials typically refers to various methods of calculating the stresses and strains in structural members, such as beams, columns, and shafts. The methods employed to predict the response of a structure under loading and its susceptibility to various failure modes takes into account the properties of the materials such as its yield strength, ultimate strength, Young's modulus, and Poisson's ratio. In addition, the mechanical element's macroscopic properties such as its length, width, thickness, boundary constraints and abrupt changes in geometry such as holes are considered.
Stress–strain analysis is an engineering discipline that uses many methods to determine the stresses and strains in materials and structures subjected to forces. In continuum mechanics, stress is a physical quantity that expresses the internal forces that neighboring particles of a continuous material exert on each other, while strain is the measure of the deformation of the material.
Thermal shock is a phenomenon characterized by a rapid change in temperature that results in a transient mechanical load on an object. The load is caused by the differential expansion of different parts of the object due to the temperature change. This differential expansion can be understood in terms of strain, rather than stress. When the strain exceeds the tensile strength of the material, it can cause cracks to form and eventually lead to structural failure.
Thermal expansion is the tendency of matter to change its shape, area, volume, and density in response to a change in temperature, usually not including phase transitions.
Micromechanics is the analysis of composite or heterogeneous materials on the level of the individual constituents that constitute these materials.
Honeycomb structures are natural or man-made structures that have the geometry of a honeycomb to allow the minimization of the amount of used material to reach minimal weight and minimal material cost. The geometry of honeycomb structures can vary widely but the common feature of all such structures is an array of hollow cells formed between thin vertical walls. The cells are often columnar and hexagonal in shape. A honeycomb shaped structure provides a material with minimal density and relative high out-of-plane compression properties and out-of-plane shear properties.
Damage mechanics is concerned with the representation, or modeling, of damage of materials that is suitable for making engineering predictions about the initiation, propagation, and fracture of materials without resorting to a microscopic description that would be too complex for practical engineering analysis.
In materials science, a composite laminate is an assembly of layers of fibrous composite materials which can be joined to provide required engineering properties, including in-plane stiffness, bending stiffness, strength, and coefficient of thermal expansion.
Firehole Composites was a supplier of computer-aided engineering (CAE) software and consulting services specializing in analysis of composite materials. Founded in 2000, the company's mission is to provide enabling technologies to further the widespread use of composite materials. Their products include Helius:MCT, Helius:CompositePro, Helius:MatSim, and Prospector:Composites.
Carbon fiber-reinforced polymers, carbon-fibre-reinforced polymers, carbon-fiber-reinforced plastics, carbon-fiber reinforced-thermoplastic, also known as carbon fiber, carbon composite, or just carbon, are extremely strong and light fiber-reinforced plastics that contain carbon fibers. CFRPs can be expensive to produce, but are commonly used wherever high strength-to-weight ratio and stiffness (rigidity) are required, such as aerospace, superstructures of ships, automotive, civil engineering, sports equipment, and an increasing number of consumer and technical applications.
Three-dimensional composites use fiber preforms constructed from yarns or tows arranged into complex three-dimensional structures. These can be created from a 3D weaving process, a 3D knitting process, a 3D braiding process, or a 3D lay of short fibers. A resin is applied to the 3D preform to create the composite material. Three-dimensional composites are used in highly engineered and highly technical applications in order to achieve complex mechanical properties. Three-dimensional composites are engineered to react to stresses and strains in ways that are not possible with traditional composite materials composed of single direction tows, or 2D woven composites, sandwich composites or stacked laminate materials.
The theory of micro-mechanics of failure aims to explain the failure of continuous fiber reinforced composites by micro-scale analysis of stresses within each constituent material, and of the stresses at the interfaces between those constituents, calculated from the macro stresses at the ply level.
HyperSizer is computer-aided engineering (CAE) software used for stress analysis and sizing optimization of metallic and composite structures. Originally developed at the US National Aeronautics and Space Administration (NASA) as ST-SIZE, it was licensed for commercial use by Collier Research Corporation in 1996. Additional proprietary code was added and the software was marketed under the name HyperSizer.
In continuum mechanics an eigenstrain is any mechanical deformation in a material that is not caused by an external mechanical stress, with thermal expansion often given as a familiar example. The term was coined in the 1970s by Toshio Mura, who worked extensively on generalizing their mathematical treatment. A non-uniform distribution of eigenstrains in a material leads to corresponding eigenstresses, which affect the mechanical properties of the material.
Digital image correlation analyses have applications in material property characterization, displacement measurement, and strain mapping. As such, DIC is becoming an increasingly popular tool when evaluating the thermo-mechanical behavior of electronic components and systems.