Search results “Mechanics and analysis of composite materials”
Composite Beam Analysis Example (Part 2) - Mechanics of Materials
An example problem solving for normal stresses due to internal moment in a simply supported composite beam using the transformed area method. Part 2 of the video covers the following topics: 1) Calculating normal stresses with flexure formula of the transformed section (or area) 2) Drawing the normal stress profile of the transformed section 3) Drawing the normal strain and stress profile of the composite section. The important part is the discussion between the relationship between the stress profile of the transformed section and the composite section.
Views: 37254 structurefree
Composite Beams Overview - Mechanics of Materials
An introduction to composite sections subject to internal bending moment. This video describes the strain and stress profile of composite sections.
Views: 59170 structurefree
Mod-05 Lec-01 Composite Materials
Processing of non metals by Dr. Inderdeep Singh, Department of Mechanical Engineering, IIT Roorkee. For more details on NPTEL visit http://nptel.iitm.ac.in
Views: 53962 nptelhrd
Pure bending of composite materials introduced
Check out http://www.engineer4free.com for more free engineering tutorials and math lessons! Mechanics of Materials Tutorial: Pure bending of composite materials introduced.
Views: 2536 Engineer4Free
Advanced Composites Analysis Failure Theories
Find out about composites analysis theories available for advanced composites analysis with NEi Nastran including: (MCT) MultiContinuum Theory Hill Hoffman Tsai-Wu Max. stress Max. strain NASA LaRC02 A video explaining PPFA (progressive ply failure analysis can also be round on YouTube, Nastran.tv or by registering for the on-demand webinar at: http://nenastran.com/advancementsinsimulation/AIS-Composite-Analysis-Advancements
Views: 10357 neisoftware
SFCM 11/12 1: Discrete damage mechanics for laminated composites
Lunes 10 de Octubre de 2011 EVER J. BARBERO - College of Engineering and Mineral Resources, West Virginia University, USA A damage constitutive model incorporated into FE commercial software is proposed for predicting onset and evolution of matrix cracking and stiffness reduction of composite laminates with otherwise arbitrary stacking sequence. Lamina crack densities are used as state variables, with crack growth driven by both mechanical and thermal stresses. Lamina moduli and critical strain energy release rates GIC and GIIC are the only properties needed for predicting both initiation and evolution of damage, without any additional adjustable parameters. Strain localization, mesh size dependence, in-situ adjustment of strength data, and/or characteristic length, are avoided by the proposed analytical stress-displacement formulation. Predicted values of crack initiation, evolution, and stiffness degradation will be presented along with to experimental data. Seminarios Internacionales de Fronteras de la Ciencia de Materiales Los Seminarios Internacionales de Fronteras de la Ciencia de Materiales son organizados por el Departamento de Ciencia de Materiales de la Universidad Politécnica de Madrid, y tienen periodicidad semanal. Su objetivo es servir de punto de encuentro, interacción y difusión de problemáticas actuales y destacadas dentro del área de la Ciencia e Ingeniería de Materiales; con una visión amplia que va desde los materiales biológicos a los materiales funcionales, pasando por aplicaciones puramente tecnológicas. En ellos se cuenta con la participación desinteresada de relevantes investigadores y tecnólogos de Universidades, Empresas y Centros de Investigación del ámbito nacional e internacional. Coordinador: Jose Ygnacio Pastor - [email protected], +34 91 336 6684
Views: 3308 UPM
UNSW - Aerospace Structures - Composites
Fibre Reinforced Materials Properties Characterisation Laminates Classical Laminate Theory Failure Prediction For educational purposes only. Although care is taken to confirm the content of these lectures, the lectures should not be used for professional engineering activities. The author and presenter of these lectures takes no responsibility for the validity of these lectures beyond what is required as a lecturer at UNSW.
Tutorial Solidworks composite plate analysis (non uniform pressure distribution)
In this video I will demonstrate how you can build your simulation using solidworks. Important: I believe that only the 2015 version have the possibility to edit larger than second degree equations. You can see more information on my blog: http://engenhariamecanicastudent.blogspot.pt/
Views: 6526 Daniel .Fonseca
Lec13, Composite beams (Lecture part 1, how to transform section)
This lecture discusses the composite beams. The method of transformed section is presented and discussed.
An Introduction to Composite Finite Element Analysis (with a modeling demonstration in Femap)
Subscribe to our channel: https://www.youtube.com/channel/UCT_qHckHnPO85O0cEpGxveQ?sub_confirmation=1 Structural Design and Analysis (Structures.Aero) is a structural analysis company that specializes in aircraft and spacecraft structures using composites. We utilize Femap, NX Nastran, Fibersim, Simcenter 3D, and HyperSizer in our analysis work and provide these programs, training, and support as a Value-Added Reseller for Siemens PLM and HyperSizer. CONNECT WITH US Join the Femap/NX Nastran User Group: https://www.facebook.com/groups/23262... Facebook: https://www.facebook.com/StructuralDe... Twitter: https://twitter.com/StructuresAero LinkedIn: https://www.linkedin.com/company/stru... Website: https://structures.aero
Transformed Area Method for Composite Beams - Mechanics of Materials
This video describes why the transformed area method is used and provides an approach to solving for normal stresses in flexural members with composites sections.
Views: 41396 structurefree
SwiftComp tutorial 2: Analysis of a Composite Box Beam
This video shows how to use Mechanics of Structure Genome to carry out composite box beam modeling. Different from the tutorial 1, material local coordinates are considered in this example. A graphic user interface is developed based on open source codes and connected to SwiftComp to carry out multiscale constitutive modeling. The software is available through https://cdmhub.org/resources/scstandard.
Views: 423 Xin Liu
Stress Analysis on Composite I-beam
Stress Analysis on Composite I-beam Voice Over: Nouha Hansen
Views: 4214 Armin Yousefi Kanani
How to solve pure bending problems for reinforced concrete
Check out http://www.engineer4free.com for more free engineering tutorials and math lessons! Mechanics of Materials Tutorial: How to solve pure bending problems for reinforced concrete. TYPO: at 7:00 I say "cubed" but write "squared." I should have written "cubed" but my hand was off doing it's own thing. That first term should be written as I said: (1/3)bx^3. Sorry for any confusion that caused.
Views: 3308 Engineer4Free
Mechanics of Composites Lab - First translaminar fracture toughness model for composites
Produced for the Mechanics of Composites Lab in the Department of Aeronautics at Imperial College London. "Using a fundamental understanding of the physical processes underlying failure of composite materials, we stand to not only to design more efficient lightweight structures, but also to design improved composite micro-structures with bespoke mechanical response. We aim to deliver world-leading research on the experimental investigation, analytical modelling and numerical simulation of the mechanical response of fibre-reinforced composite materials. Our group consists of passionate, creative and committed researchers, which pursue excellence on every aspect of their research." By noticing the key role played by hierarchy in the fibre tensile failure mode in UD plies, the group developed the first analytical model in the literature that is capable of predicting the translaminar fracture toughness of UD plies. This model can be used not only for structural design, but also for material development, since the predictions are obtained from fibre / matrix / interface properties.
Views: 747 Ben Lucas-Lee
Modeling Progressive Damage on Composite Plate
Modeling Progressive Damage on Composite Plate. The user is familiar with • Standard workflow in ANSYS Workbench and ANSYS Composite PrePost • Composite Solid Modeling • Basics of Composite Engineering For full ACP tutorials please click on this link : https://www.udemy.com/ansys-tutorial/?couponCode=STUDENT
Views: 10382 Armin Yousefi Kanani
Analysis tool for short fiber composites.mp4
This tool is developed by HSCL in South Korea, aimed at predicting the stress-strain behavior of short fiber structures. The core theory is based on micro-mechanics of failure (MMF).
Views: 912 Lei Xu
Webinar: Progressive Failure Analysis in laminate composites
Learn how to run Progressive failure analysis in an NX environment using Abaqus solver. You will also learn about how to create new user-defined materials UMATs and how to integrate them in NX.
Mechanics of Composites Lab - First Ply-Level Translaminar Fracture Toughness Test
Produced for the Mechanics of Composites Lab in the Department of Aeronautics at Imperial College London. "Using a fundamental understanding of the physical processes underlying failure of composite materials, we stand to not only to design more efficient lightweight structures, but also to design improved composite micro-structures with bespoke mechanical response. We aim to deliver world-leading research on the experimental investigation, analytical modelling and numerical simulation of the mechanical response of fibre-reinforced composite materials. Our group consists of passionate, creative and committed researchers, which pursue excellence on every aspect of their research." - Dr Silvestre Pinho, Lab Leader. Home Contributions Projects Recognition People Constitutive Models Fracture Toughness Test Fracture Toughness Model Recycled Composites Numerical Models Periodic boundary conditions Translaminar fracture of a composite UD ply leads to energy being dissipated by splitting (a form of matrix cracking), friction (during the pull-out of fibres), fibre fracture (which is counter-institutively negligible at least in most cases), as well as local delamination. While the fracture surface is complex at he microscopic level, from a mesoscopic point of view it is possible to regard the fracture surface as a homogenised fracture plane. The question then becomes: what should the fracture energy associated with the formation of this fracture plane be? The answer to this question is relevant for numerical models that include these homogenised cracks and for the comparison of different material systems. In 2002-2004, when developing the first regularised smeared-crack model for laminated composites, the group needed ply-level translaminar fracture toughness values. At the time, these toughnesses did not exist even as a concept. Since then, the group has developed and perfected experimental tests to measure translaminar toughness in tension and compression, for UD and woven plies, for plies with fibres at an angle, and the group has demonstrated how the toughness depends on the thickness of the plies. Music - Primeva - Einaudi
Views: 3789 Ben Lucas-Lee
Analysis of composite model part 2/2
Part 1 Analysis in Ansys Workbench and ACP (model 2D) Part 2 Analysis in ACP (model 3D)
Views: 5917 friedrichpiotr
Fiber, Matrix, and Porosity Analysis in a Polymer Matrix Composite
The structure and properties of polymers are becoming increasingly important as they are used in structural applications, both on their own and in polymer matrix composites (PMCs). Robo-Met.3D®, an automated serial sectioning system, provides 2D optical microstructural data for 3D characterization of microstructural features such as size, shape and distribution of matrix materials, strengthening fibers, and porosity. Check out this application note about the serial sectioning analysis of a PMC with a high temperature thermosetting resin matrix and a imide-based fiber reinforcement: https://www.ues.com/forums/topic/3d-characterization-of-fiber-orientation-in-a-polymer-matrix-composite/
Views: 360 UES, Inc.
Professor Park, Mechanical Engineering
Professor Dr. Seungbae (SB) Park is doing incredible research in a number of areas, including: Strength of materials, mechanics of composite materials, facture mechanics, finite element analysis I and II . Physical reliability of small-scale systems such as MEMS and sensors, advanced packaging solution in 3-D packaging and Pb-free solders, optomechanics in micro scale deformation analysis and reliability of structural failure. Hear him discuss his research and the kinds of students he hopes to work with in these areas. http://www.binghamton.edu/watson/ Video by Prentice Studios
Strength of Materials: Analysis of shearing stress
Want to see all of Dr. Jawa's engineering mechanics videos (statics, dynamics, strength of materials)? https://www.youtube.com/playlist?list=PLZOZfX_TaWAEzhyvNT1e9jbmTt4Eqo8C0 Want to see more mechanical engineering instructional videos? Visit the Cal Poly Pomona Mechanical Engineering Department's video library, ME Online (http://www.cpp.edu/meonline).
Views: 93727 CPPMechEngTutorials
Ply Mechanics: Stress-Strain Relations
Stress strain relations in composite materials #WikiCourses http://wikicourses.wikispaces.com/Topic03+Ply+Mechanics
Views: 433 Mohammad Tawfik
Composite Beams
Analysis of a composite beam made of a steel channel with a wooden insert. This goes over use of the transformation factor to convert the wooden member into a mechanically equivalent steel member.
Views: 4748 jdomann
Shear Flow Example - calculate connector spacing - Mechanics of Materials
This is a video that provides and explanation of built-up shapes (first 5 minutes) and provides a detailed example of applying the shear flow relationships to determine the maximum spacing of screws for a built-up I beam. 0:00 - Overview of shear flow and built-up shapes 5:07 - Start of example problem 9:00 - Shear Diagram 11:30 - Basic design relationship with shear flow equation 15:51 - Calculating I, moment of inertia 18:04 - Calculating Q, first moment of area 24:13 - Solving for the maximum spacing
Views: 56722 structurefree
The History of Composite Analysis and NEi Nastran
The video reviews the complexity of analyzing composite materials, history of composite failure theories and how it relates to the NEi Nastran engine. NEi Software started incorporating composite materials analysis in the NEi Nastran code in 1995 and is a leader in composite analysis software development today. See the history, the partnerships and join our 20 Years of FEA celebration at 20YearsofFEA.com. A special thank you to Ravin Kumar and Jennifer Miller for their physical testing footage.
Views: 1190 neisoftware
Experimental Mechanics: Projectile Impact on a Composite Material
Infrared Imaging of a Projectile Impact on a Composite Material Plate
Views: 177 Telops
Principle of Superposition of Forces/mos/gtu
in this video i show you how to solve numericals about principle of superposition of forces................
Views: 30563 GTU MIMP
NFX Technical Webinar: Composite Material usage and Theory
This is a specialist level training webinar for users of midas NFX and all Engineers who want to learn more about FEA Analysis. This is an advanced webinar about composite materials usage and definition in midas NFX. During the webinar you will learn about: Types of composite materials Definition of 2D/3D composite material in midas NFX Types of Failure criteria Visualization of ply results Composite board analysis We will have a special guest during this webinar: Matteo Vettori from e-FEM (phD in composite materials) in Italy who will talk about his own experience with composite material in midas NFX. You can even ask your questions in direct at the end of the webinar ! It is free, you have nothing to lose by joining ;-) Hope to see you soon
Views: 3228 Cyprien Rusu
Composite Materials Overview for Engineers | UWashingtonX on edX | About Video
Composite Materials Overview for Engineers Register for Composite Materials Overview for Engineers at https://www.edx.org/courses Introduction of composite materials from engineering design, manufacturing, and repair viewpoints. About this Course Composites are used in many industries today to enable high-performance products at economic advantage. These industries range from space to sports and include manufactured products for aircraft, transportation, energy, construction, sports, marine, and medical use. There are many material, economic and aesthetic advantages to using composites, but a solid knowledge of the physical properties, including the mechanics, tooling, design, inspection & repair, and manufacturing options is required for working in this medium as they are intrinsically linked. This course provides an introduction to the fundamentals of composite materials for high performance structures from the point of view of Aerospace engineering design, manufacturing, and repair. It is designed to address critical areas of composite technologies that focus on materials, manufacturing, mechanics, design, inspection, and repair. In this course students will learn how composite materials achieve properties of strength, weight ratios and durability that surpass aluminum in aircraft design. For these high performance applications engineers typically rely on laminated structures, which are built up from many varying layers of ply-materials. Using this process the mechanical properties of the composite part can be tailored to specific applications resulting in significant weight and cost savings. Tailoring specific properties and designing innovative laminate structures highlights the multidisciplinary nature of this industry and how it touches the expertise of many disciplines including engineers, mechanics, and inspection specialists. After successfully completing this course, students will be able to identify the unique characteristics of composites and understand how advanced composite structures are designed, manufactured and maintained. When you have finished this course, you will be able to: Demonstrate understanding of fundamentals in materials, manufacturing, mechanics, design, and repair of polymeric matrix composites Identify advantages and disadvantages of polymeric matrix composites with respect to metals Apply the knowledge acquired to the design and manufacturing of high performance composite structures
Views: 26659 edX
SolidWorks Simulation Tutorial - Composit Carbon Fiber Tubes (Orthotropic material)
Simulation Tutorial of orthotropic materials (carbon fiber).
Views: 15643 rcBlackFalcon
Thermal stress (GATE Lecture)
In this video we have explained the concept of stresses and strains due to thermal effects in a very easy manner. Click here to buy our book of Strength of Materials on Flipkart https://bit.ly/MosGATE
Views: 24300 GateMentor

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