February 20th - April 3rd, 2018
07:00 PST / 10:00 EST / 15:00 GMT / 16:00 CET
Five-Session Live Online Training Course - 2 hours per session
Attend the live sessions, or view the recordings at your convenience
PLEASE NOTE THAT DAYLIGHT SAVINGS TIME WILL AFFECT THE TIMING OF SOME OF THE SESSIONS IN THIS COURSE.
FULL DETAILS WILL BE PROVIDED UPON REGISTRATION.
This 5-session, live online course will cover a range of topics, all aimed at structural designers and engineers.
You can either attend the live sessions or
take the course on-demand at your leisure.
NAFEMS e-learning gives you the best of both worlds, giving you real, practical knowledge that you can use day-to-day to improve your analyses.
Composite systems include many more factors than conventional metallic structures.
The objective of this course is to break down the composite analysis process into clearly defined steps, give an overview of the physics involved and show how to successfully implement practical solutions using Finite Element Analysis.
Moving to composite structures will allow you to explore:
Composite materials span:
The challenge for the designer and analyst is to make decisions on the type of idealization and level of detail required in the Finite Element Analysis. Your design may include:
Analysis is further complicated by:
We can help you plan a strategy for dealing with these challenges.
Note: homework is purely voluntary!
All attendees on the course will be able to download a fully functioning Composite Stiffness and Strength Calculator, together with user guide.
Many past attendees have found this tool a useful supplement to post processing available in their usual Finite Element solution. Attendees will be entitled to future upgrades.
Students will join the audio portion of the meetings by utilizing the VoIP (i.e. headset connected to the computer via headphone and microphone jacks) or by calling into a standard toll line. If you are interested in additional pricing to call-in using a toll-free line, please send an email to: e-learning @ nafems.org .
Note: This is a five-session course. Each session represents one 2-hour session per week.
Telephony surcharges may apply for attendees who are located outside of North America, South America and Europe. These surcharges are related to individuals who join the audio portion of the web-meeting by calling in to the provided toll/toll-free teleconferencing lines. We have made a VoIP option available so anyone attending the class can join using a headset (headphones) connected to the computer. There is no associated surcharge to utilize the VoIP option, and is actually encouraged to ensure NAFEMS is able to keep the e-Learning course fees as low as possible. Please send an email to the e-Learning coordinator (e-learning @ nafems.org ) to determine if these surcharges may apply to your specific case.
Just as with a live face-to-face training course, each registration only covers one person. If you plan to register a large group (10+), please send an email to e-learning @ nafems.org in advance for group discounts.
For NAFEMS cancellation and transfer policy, click here.
|MASco2||Explain the terms Isotropic, Orthotropic, Anisotropic and Homogeneous.|
|CMPSkn1||List the various steps in the analysis/simulation process and identify those requiring particular consideration due to the inherent nature of the composite material / structure.|
|CMPSkn2||Define the meaning of membrane/bending coupling and outline the circumstances in which this can occur.|
|CMPSkn3||List the various failure criteria available in any system used.|
|CMPSkn4||Identify the laminated elements available in any system used, highlighting any developer preferences.|
|CMPSco1||Discuss the sources of approximation inherent in finite element analysis of composite materials and structures.|
|CMPSco2||Describe the approximate post-processing method used with some elements to obtain inter-ply shear and normal stresses.|
|CMPSco3||Discuss approximations relating to fibre direction in curved shell models.|
|CMPSco4||Explain how manufacturing methods can lead to fibre direction and volume fraction variations from the "as-specified" or "ideal".|
|CMPSco5||Discuss the difficulties that can arise in using symmetry techniques and plane stress/strain assumptions.|
|CMPSco6||Discuss the various failure mechanisms in composite materials.|
|CMPSco7||Discuss the difficulties inherent in conducting analyses involving damage progression.|
|CMPSco9||Outline how element stiffness matrices are evaluated for laminated elements.|
|CMPSco10||Explain the term free edge effect.|
|CMPSco13||Explain the terms cross-ply, unidirectional, unsymmetric and balanced.|
|CMPSco14||Discuss the ABD matrix.|
|CMPSco15||Explain the terms drape and bias.|
|CMPSco16||Explain the terms weft and weave.|
|CMPSco18||Explain the terms gel coat and pre-preg.|
|CMPSco19||Discuss the general roles of fibre and matrix in a composite.|
|CMPSco21||Discuss scenarios where a Representative Volume Element modelling approach would be appropriate.|
|CMPSco22||Discuss some possible analysis consequences of utilising a laminate with an unsymmetrical/anti-symmetric lay-up.|
|CMPSco24||Contrast the relative significance of transverse shearing effects for composites and isotropic homogeneous materials.|
|CMPSco25||Explain the term quasi-isotropic and illustrate a laminate specification where this might be a reasonable assumption.|
|CMPSco26||Explain the purposes of the skins and core in a sandwich construction.|
|CMPSap1||Complete laminate definitions, using stacking notation, for a range of materials and lay-ups.|
|CMPSap2||Illustrate the approximate nature of finite element analysis, through examples chosen from your industry sector or branch of engineering.|
|CMPSap3||Illustrate situations where use of an equivalent orthotropic idealisation may be appropriate.|
|CMPSap4||Use laminated shells and bricks effectively in small displacement, linear elastic FEA.|
|CMPSap5||Use sandwich elements effectively in small displacement, linear elastic FEA.|
|CMPSap6||Use laminated shells and bricks effectively in nonlinear FEA.|
|CMPSan3||Employ draping software, where applicable.|
|CMPSan4||Employ Laminate Analysis Software as a complimentary tool where appropriate.|
|CMPSsy3||Plan a series of simple benchmarks in support of a composite analysis.|
|CMPSev1||Select appropriate idealisations for typical industry components/structures, which are consistent with the objectives of the analyses.|
|CMPSev2||Specify appropriate failure criteria for a range of analyses.|
|MSAkn1||Define Multiscale Analysis.|
|MSAkn7||Define and list the classical approaches to multi-scale analysis.|
|MSAco3||EComposite FEAplain continuum theory and why continuum methods cannot be used at the atomistic scale.|
|MSAco12||Describe the trends in hardware and software and how these will impact on current multi-scale analysis procedures.|
Not Available to Attend this Time?
Would you like us to notify you when the next run of this course is open for enrollment? If so, add yourself to the eLearning Waitlist!
Note: Once you register for the course using the "order" button (look up), you will receive your invoice, and the day before the course starts, an email invite to the class discussion board. Please note that no 'physical' goods will be mailed to you.
Please click here to view the FAQ section, or if you need to contact NAFEMS about this course.
Engineering Board PDH Credits
*It is your individual responsibility to check whether these e-learning courses satisfy the criteria set-out by your state engineering board. NAFEMS does not guarantee that your individual board will accept these courses for PDH credit, but we believe that the courses comply with regulations in most US states (except Florida, North Carolina, Louisiana, and New York, where providors are required to be pre-approved).