Example 2: Lagrangian modeling for an impact problem 1 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2.

Slides:



Advertisements
Similar presentations
Rotational Inertia. Circular Motion  Objects in circular motion have kinetic energy. K = ½ m v 2  The velocity can be converted to angular quantities.
Advertisements

Absorptive Muffler with Shells
Moment of Inertia. Moment of Inertia Defined  The moment of inertia measures the resistance to a change in rotation. Change in rotation from torqueChange.
Chapter 9 Linear Momentum and Collisions. Linear momentum Linear momentum (or, simply momentum) of a point-like object (particle) is SI unit of linear.
FEA of a Golf Driver and Golf Ball
EMA D Elements. Introduction 3-D elements have 3 degrees of freedom per node (u x, u y, u z ) The two fundamental shapes are hexahedral and tetrahedral.
Review of existing numerical methods and validation procedure available for bird strike modelling Review of existing numerical methods and validation procedure.
Chapter 10 Review Bingo. DIRECTIONS  Fill in the answers listed on the board anywhere on your Bingo card.  You will not have a FREE SPACE.
FE analysis with bar elements E. Tarallo, G. Mastinu POLITECNICO DI MILANO, Dipartimento di Meccanica.
DID YOU KNOW: slender or thin structures can be modelled with Shells in ANSYS? Consider a flat plate of dimensions 6m x 6m x 0.002m (thick); evaluate the.
Introduction to ABAQUS 27 th February, Units Before starting to define any model, you need to decide which system of units you will use. ABAQUS.
Fracture and Fragmentation of Thin-Shells Fehmi Cirak Michael Ortiz, Anna Pandolfi California Institute of Technology.
Theory of Elasticity Theory of elasticity governs response – Symmetric stress & strain components Governing equations – Equilibrium equations (3) – Strain-displacement.
Lecture 34, Page 1 Physics 2211 Spring 2005 © 2005 Dr. Bill Holm Physics 2211: Lecture 34 l Rotational Kinematics çAnalogy with one-dimensional kinematics.
Physics 151: Lecture 20, Pg 1 Physics 151: Lecture 20 Today’s Agenda l Topics (Chapter 10) : çRotational KinematicsCh çRotational Energy Ch
Chapter 7 Impulse and Momentum.
1 Kul Finite element method II – Vibration of a four storey building.
FE Modeling Strategy Decide on details from design Find smallest dimension of interest Pick element types – 1D Beams – 2D Plate or.
Shell Elements Jake Blanchard Spring Shell (or plate) Elements These are typically “planar” elements They are used to model thin structures which.
AEROELASTIC MODELING OF A FLEXIBLE WING FOR WIND TUNNEL FLUTTER TEST WESTIN, Michelle Fernandino; GÓES, Luiz Carlos Sandoval; SILVA, Roberto Gil Annes.
Geometry Jeopardy! Ch 1-6 Formulas & Definitions SA of Prisms & Cylinders SA of Cones & Pryamids Volume of Prisms & Cylinders Volume of Cones & Pyramids.
A 1 LS-DYNA geometry for the DRDC experiment. *Test performed by Defence R&D Canada, Williams et. Al. SPH C4 Charge 5 cm DOB 8 cm thick 12.5 cm radius.
Simulation of Roll Forming
Copyright © 2010 Altair Engineering, Inc. All rights reserved.Altair Proprietary and Confidential Information Section 13 Loads and Boundary Conditions.
Cubes, Prisms, Pyramids, Cylinders, Cones and Spheres
Physics 111 Practice Problem Statements 09 Rotation, Moment of Inertia SJ 8th Ed.: Chap 10.1 – 10.5 Contents 11-4, 11-7, 11-8, 11-10, 11-17*, 11-22, 11-24,
Chapter 10 Review Bingo.
Example Problem The parallel axis theorem provides a useful way to calculate I about an arbitrary axis. The theorem states that I = Icm + Mh2, where Icm.
Circles and Projectiles. 1 - Motion in Two Dimensions 2 - Circular Motion 3 - Centripetal Force, Gravity, and Orbits 4 - Center of Mass.
Copyright © 2010 Altair Engineering, Inc. All rights reserved.Altair Proprietary and Confidential Information Section 16 Rigid Connections.
Copyright © 2010 Altair Engineering, Inc. All rights reserved.Altair Proprietary and Confidential Information Section 4 Applications.
Fan Blade Analysis By Andrew Hinthorn. Background Model an aluminum fan blade in Pro/E Conduct stress analysis on the blade using Visual Nastran.
Physics 1501: Lecture 19, Pg 1 Physics 1501: Lecture 19 Today’s Agenda l Announcements çHW#7: due Oct. 21 l Midterm 1: average = 45 % … l Topics çRotational.
PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY
A Study of the Effect of Imperfections on Buckling Capability in Thin Cylindrical Shells Under Axial Loading Lauren Kougias.
Physics.
9 rad/s2 7 rad/s2 13 rad/s2 14 rad/s2 16 rad/s2
Physics 111: Lecture 17, Pg 1 Physics 111: Lecture 17 Today’s Agenda l Rotational Kinematics çAnalogy with one-dimensional kinematics l Kinetic energy.
Wednesday, Oct. 22, 2003PHYS , Fall 2003 Dr. Jaehoon Yu 1 PHYS 1443 – Section 003 Lecture #15 Wednesday, Oct. 22, 2002 Dr. Jaehoon Yu 1.Impulse.
The Laws A section in the chapter of the study of Dynamics of motion.
Sect. 10.4: Rotational Kinetic Energy
4.1 Rotational kinematics 4.2 Moment of inertia 4.3 Parallel axis theorem 4.4 Angular momentum and rotational energy CHAPTER 4: ROTATIONAL MOTION.
Momentum p = m v Momentum = mass * velocity momentum is directly proportional to an object's mass momentum is directly proportional to the object's velocity.
ME 498CM Fall 2015 Loading & Analysis.
ADAMS Assignment 2 ME451:Kinematics and Dynamics of Machine Systems (Fall 2013) Assigned: October 2, 2013 Due: October 9, 2013.
GEOMETRY IN MY LIFE BY AMANDA HORTON. CIRCLE A circle is a round shape with no edges points this shape has 1 face.
CHAPTER 10 - LAGRANGIAN BOUNDARY CONDITIONS
Sample Dimensions 17mm x 6.5mm x 1mm Inlet Outlet Moving posts Fixed posts Direction of linear motion.
Wednesday, June 20, 2007PHYS , Summer 2007 Dr. Jaehoon Yu 1 PHYS 1443 – Section 001 Lecture #12 Wednesday, June 20, 2007 Dr. Jaehoon Yu Impulse.
Wednesday, July 7, 2004PHYS , Summer 2004 Dr. Jaehoon Yu 1 PHYS 1441 – Section 501 Lecture #11 Wednesday, July 7, 2004 Dr. Jaehoon Yu Collisions.
S TRESS A NALYSIS OF A H YDRAULIC A CTUATOR B ASED ON A CCUMULATOR R ESPONSE By John Connor Ernesto Gutierrez-Miravete, Thesis Adviser.
Appendix A.
ABSOLUTE MOTION ANALYSIS Today’s Objective: Students will be able to: 1.Determine the velocity and acceleration of a rigid body undergoing general plane.
UT-BATTELLE New method for modeling acoustic waves in plates A powerful boundary element method is developed for plate geometry The new method achieves.
Dynamics FE Review Session Adapted from the following references:
Divide into meridian sections – Gore development
Rolling Motion. Rolling Motion Rolling Motion If we separate the rotational motion from the linear motion, we find that speed of a point on the outer.
ENFORCED MOTION IN TRANSIENT ANALYSIS
Rotational Inertia.
326MAE (Stress and Dynamic Analysis) 340MAE (Extended Stress and Dynamic Analysis)
9.8 Momentum and Kinetic Energy in Collisions
Solid Geometry.
Center of Mass & Linear Momentum
Conservation of momentum
Newton’s Laws.
How do we find the center of mass of a system?
FAA/GMU Project Development of AL MAT224 Dataset (V2.0)
Solid Geometry.
Water Strider Body Segment Dimensions Contact Perimeter (mm)
Solid Geometry.
Presentation transcript:

Example 2: Lagrangian modeling for an impact problem 1 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2

2 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY Direct impact problem A rigid body (5 kg) with 50 m/sec impacts on the aluminum plate.  Aluminum plate Dimensions: 1m× 1m× 0.002m Material type: Linearly elastic behavior with isotropic hardening Element : Shell elements (S4R) Mesh size: 0.01m-0.05m Boundary condition: Four edges are fully constrained.  Rigid body impactor Shape: cylinder with two hemispherical caps Dimensions: 0.32 in length × 0.16 m in a diameter Length/ diameter = 2 Initial bird mass: 5 kg Magnitude of initial velocity: VZ = -50 m/s Rigid elements (R3D4)

3 EXAMPLE 2 Target structure Model type: Shell model Shape: Square plate Dimensions: 1m× 1m PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY

4 EXAMPLE 2 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY Reference geometry for an Impactor Model type: Discrete rigid model Shape: Cylinder with hemispherical cap and straight end Dimensions: 0.16 m in a diameter × 0.32 m in length

5 EXAMPLE 2 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY

6 EXAMPLE 2

7 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2 Coordinate (0,0,0) Coordinate (0.5, 0.5, 0.01)

8 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2

9 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2

10 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2

11 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2

12 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2

13 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2

14 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2 Animation

15 PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2 Target: 0 <X < 0.8 Animation

Lagrangian modeling is very traditional, available  ABAQUS 6.12 documentation: Abaqus Analysis User's Manual “Rigid elements,” Section 30.3  ABAQUS 6.12 documentation: Abaqus Example Problems Manual “Rigid projectile impacting eroding plate,” Section PREPARED BY NORI. NANAMI, TEXAS A & M UNIVERSITY EXAMPLE 2