Status Update-Backed Tests vs. Simulation Comparison

Slides:



Advertisements
Similar presentations
Lecture #13 Properties of Hardening Concrete Curing.
Advertisements

Evaluation of Cracking Resistance of Superpave Mixtures Using Texas Overlay Test Syeda Rubaiyat Aziz Mustaque Hossain Greg Schieber Department of Civil.
Finite Element Study of Bond-Slip Behaviour of CFRP and GFRP Laminates on Brick Masonry Candidate:Chi Chiu Lam Supervisors:Prof. M. R. Valluzzi Dr. E.
An Experimental Study and Fatigue Damage Model for Fretting Fatigue
Finite Element Simulation of Woven Fabric Composites B.H. Le Page *, F.J. Guild +, S.L. Ogin * and P.A. Smith * * School of Engineering, University of.
Computer-Aided Engineering Design
Dynamic axial crush response of circular honeycombs by Royan J. D'Mello, Sophia Guntupalli, Lucas R. Hansen, and Anthony M. Waas Proceedings A Volume ():rspa
MSE 201 – Laboratory IThe University of Tennessee Materials Science and Engineering Kurt Johanns MSE Laboratory I Mechanical Properties of Metals.
Chapter 17 Design Analysis using Inventor Stress Analysis Module
Prediction of Load-Displacement Curve for Weld-Bonded Stainless Steel Using Finite Element Method Essam Al-Bahkali Jonny Herwan Department of Mechanical.
A U.S. Department of Energy Office of Science Laboratory Operated by The University of Chicago Argonne National Laboratory Office of Science U.S. Department.
A servo controller for an MTS machine Characterization Presentation David Schwartz & Uri goldfeld Supervisors : Dany Alkalay & Mony Orbach.
LMAF / EPFL What's new? Tested 9 specimens (3 plates, 1mm joint): 2 cameras -> local / global deformations 2 cameras -> local / global deformations variability.
Napoli - 21 February 2004 – Simone Merlin SLIDE 1 Analysis of the hidden terminal effect in multi-rate IEEE b networks Simone Merlin Department of.
Characterization of 1mm lead-free joints. Test results (DIC 2D)
COMPUTER-AIDED DESIGN The functionality of SolidWorks Simulation depends on which software Simulation product is used. The functionality of different producs.
Mechanics of Materials Goal:Load Deformation Factors that affect deformation of a structure P PPP Stress: intensity of internal force.
The UNIVERSITY of NORTH CAROLINA at CHAPEL HILL Adaptive Weighted Deconvolution Model to Estimate the Cerebral Blood Flow Function in Dynamic Susceptibility.
Plate and shell elements All the following elements enable to create FE mesh of a thin-walled body, with the thickness being one of the important input.
Anisotropy of Commercially Pure Titanium (CP-Ti) Experimental Setup and Procedures Experimental Results Results and Conclusions Project Objective: To assess.
Department of Aerospace and Mechanical Engineering A one-field discontinuous Galerkin formulation of non-linear Kirchhoff-Love shells Ludovic Noels Computational.
Engineering Doctorate – Nuclear Materials Development of Advanced Defect Assessment Methods Involving Weld Residual Stresses If using an image in the.
Operated by Los Alamos National Security, LLC for the U.S. Department of Energy's NNSA | UNCLASSIFIED | 1 Post Irradiation Examination of an Alloy 718.
14th Crisp user meeting at UCL1 Numerical analysis of a piled foundation in granular material using slip element Yongjoo Lee Soil Mechanics Group Department.
Comparison of HIP and VPS Tungsten Coating Behavior Using Laser Spallation Jaafar El-Awady with significant contributions from H. Kim, J. Quan, S. Sharafat,
Materials Process Design and Control Laboratory Finite Element Modeling of the Deformation of 3D Polycrystals Including the Effect of Grain Size Wei Li.
Evaluation of Residual Stresses due to Spherical Impact using LS – DYNA Jason Fayer MANE-6980 ENGINEERING PROJECT Spring 2010 Status Update.
Dynamic Behaviour of Unsaturated CH soil under Cyclic Loading in Unconsolidated Undrained Conditions 5th Tongji-UBC Symposium on Earthquake Engineering,
`` Solid DT Studies - Update presented by John Sheliak - GA Drew A. Geller, & James K. Hoffer - LANL presented at the 16th High Average Power Laser Workshop.
Evaluation of Residual Stresses due to Spherical Impact using LS – DYNA Jason Fayer MANE-6980 ENGINEERING PROJECT Spring 2010.
Heat load of the radiation cooled Ti target of the undulator based e+ source Felix Dietrich (DESY, TH-Wildau),Sabine Riemann(DESY), Andriy Ushakov(U- Hamburg),
MECH 322 Instrumentation Lab 5 Elastic Modulus of an Aluminum Beam Performed: February 9, 2004 Sinan Ozcan: I believe I performed 50% of the work for this.
GIGATRACKER SUPPORTING PLATE COOLING SYSTEM SIMULATION 1Vittore Carassiti - INFN FECERN, 11/12/2007.
Explicit-to-Implicit Sequential Solution
Modeling Procedure SOLID186 – Ten-Noded Tetrahedral 198 Elements 5247 Elements *Needed mid-nodes to model curves.
February 5, Fatigue of Asphalt Mixtures, Endurance Limit, Polymer Modifications, Healing 1.E+02 1.E+03 1.E+04 1.E+05 1.E-07 1.E-05 1.E-03 1.E-01.
Simulation of Phase transformation behavior of NiTi doped with Cu during loading using classical molecular dynamics S. Aich, A. Behera and S. Ghosh Department.
Mechanical & Aerospace Engineering West Virginia University Elastic Properties of Materials, Tensile Test Xingbo Liu.
The information contained in this document is GKN Aerospace Sweden AB Proprietary information and it shall not – either in its original or in any modified.
Date of download: 6/22/2016 Copyright © ASME. All rights reserved. From: Plastic Limit Loads of Pad Reinforced Cylindrical Vessels Under Out-of-Plane Moment.
EFFECT OF FLANGE LENGTH AND BLANK HOLDER FORCE ON CRACK INITIATION IN STRETCH FLANGING PROCESS  S. K. Panthia*, Yogesh Dewangb, M. S. Horab, Meraj Ahmeda.
Date of download: 10/1/2017 Copyright © ASME. All rights reserved.
Lagouge TARTIBU KWANDA Mechanical Engineering
Additive Manufacturing of Bio-Inspired Mechanical Interlocking
Mickaël MULLER, Evelyne TOUSSAINT and Michel GREDIAC
UNIVERSITY OF NAIROBI DEPARTMENT OF MECHANICAL AND MANUFACTURING ENGINEERING ENGINEERING DESIGN II FME 461 PART 5 GO NYANGASI November 2008.
Inconel 718 & Ti6Al4V Update Status Update Jarrod Smith Jeremy Seidt
Simulated elliptical bioprosthetic valve deformation: Implications for asymmetric transcatheter valve deployment  Wei Sun, Kewei Li, Eric Sirois  Journal.
Status Update-Sequentially Loaded Backed Tests
NSM LAB Net Shape Manufacturing Laboratory
From: Effect of High Strain Rate on Indentation in Pure Aluminum
APPLICATION OF COHESIVE ELEMENT TO BIMATERIAL INTERFACE
Date of download: 11/6/2017 Copyright © ASME. All rights reserved.
Explicit Methods in Quasi-Static Analyses of Rubber-Like Materials
FRESCA2 Update on the dipole design and new calculations
The projectile shape and material effect on the momentum transfer for asteroid orbit change Daisuke Yokoo, Masashi Tanaka, Masaya Ikeda, Takao Koura and.
Date of download: 1/3/2018 Copyright © ASME. All rights reserved.
Date of download: 1/13/2018 Copyright © ASME. All rights reserved.
Elongation at break membrane testing procedure according to ASTM D 412
DEPARTMENT OF MECHANICAL AND MANUFACTURING ENGINEERING
Flexible pavement design
Reservoir Simulation FEEDBACK INPUT Geologic Model Time
Visco-plastic self-consistent modeling of high strain rate and
FAA/GMU Project Development of AL MAT224 Dataset (V2.0)
DEPARTMENT OF MECHANICAL AND MANUFACTURING ENGINEERING
RADIATION AND COMBUSTION PHENOMENA
LABORATORY OF PROCESS ENGINEERING
Tutorial.
Experimental Mechanics - assignment
Figure 1 True strain, e.
Presentation transcript:

Status Update-Backed Tests vs. Simulation Comparison Department of Mechanical & Aerospace Engineering Dynamic Mechanics of Materials Laboratory Status Update-Backed Tests vs. Simulation Comparison Nathan Spulak February 16, 2017 1 1

Simulation Mesh Size vs. Test VSGL Department of Mechanical & Aerospace Engineering Dynamic Mechanics of Materials Laboratory Mesh Size Comparison Simulation Mesh Size vs. Test VSGL Test Scenario 3D Simulation Mesh Size (mm) Average VSGL (mm) Unbacked 0.12 0.255 0.05” Backer, 0.089” Punch 0.07 0.269 0.1” Backer, 0.063” Punch 0.26904 2 2

Strain Data from Area of Interest Department of Mechanical & Aerospace Engineering Dynamic Mechanics of Materials Laboratory Strain Data from Area of Interest Find number of strain values within the target area of interest 3 3

Strain Data from Area of Interest Department of Mechanical & Aerospace Engineering Dynamic Mechanics of Materials Laboratory Strain Data from Area of Interest Test Scenario DIC # Points/Area [points/mm2] Target Area [mm2] # Points in Target Area (approximate) Unbacked 351.55 ε1≥0.02 , Area=44.33 15,583 ε1≥0.19 , Area=0.687 241 0.05” Backer, 0.089” Punch 398.0 ε1≥0.02 , Area=89.75 35,719 *Note: DIC values taken from backing plate, not specimen ε1≥0.19 , Area=0.2297 91 0.1” Backer, 0.063” Punch 377.3 ε1≥0.02 , Area=138.1 52,103 ε1≥0.19 , Area=2.861 1,079 4 4

Load-Displacement Curve Comparison Department of Mechanical & Aerospace Engineering Dynamic Mechanics of Materials Laboratory Load-Displacement Curve Comparison 5 5

Annealed Cu Testing Data Department of Mechanical & Aerospace Engineering Dynamic Mechanics of Materials Laboratory Annealed Cu Testing Data 0.125” Annealed Cu (Machined to 0.1” thick for backing plate) 0.05” Annealed Cu 7 7

Dynamic Mechanics of Materials Laboratory Department of Mechanical & Aerospace Engineering Dynamic Mechanics of Materials Laboratory Next Steps: Input test data from Cu into DYNA, see how that affects simulation results Proceed with Sequentially Loaded Backed Tests Continue new experiment designs to obtain triaxialities between -1/3 and +1/3 along Lode=-1 8 8