Statistical Optimization and Structural Analysis: Design of handmade custom Snowboards. Benoit CAILLAUD

Similar documents
ON THE INFLUENCE OF CHANGING SNOW PROPERTIES ONTO THE STRUCTURAL BEHAVIOUR OF A SNOWBOARD UNDERGOING A CARVED TURN

Computational Analysis for Composites

Comparison of Ply-wise Stress-Strain results for graphite/epoxy laminated plate subjected to in-plane normal loads using CLT and ANSYS ACP PrepPost

Finite element modelling of infinitely wide Angle-ply FRP. laminates

Flexural properties of polymers

Effect of Specimen Dimensions on Flexural Modulus in a 3-Point Bending Test

MarkForged's Onyx is a material that is ideal for customer-facing parts that need to look good while standing up to industrial requirements.

INDUSTRIAL FORMING SIMULATION OF MULTI-LAYERED UD NON-CRIMP-FABRICS. 13. LS-DYNA FORUM, , BAMBERG.

Effects of Resin and Fabric Structure

Dynamic analysis of Composite Micro Air Vehicles

Composite models 30 and 131: Ply types 0 and 8 calibration

Bending of Simply Supported Isotropic and Composite Laminate Plates

QUESTION BANK Composite Materials

Mechanical Behavior of Composite Tapered Lamina

DRAPING SIMULATION. Recent achievements and future trends. Dr. Sylvain Bel LGCIE University Lyon 1

Rigid pavement design

Dynamic Response Of Laminated Composite Shells Subjected To Impulsive Loads

Machine Direction Strength Theory of Corrugated Fiberboard

Dynamic Responses of Composite Marine Propeller in Spatially Wake

PRESSURE VESSELS & PRESSURE CABINS FOR BLENDED WING BODIES

Impact and Crash Modeling of Composite Structures: A Challenge for Damage Mechanics

SANDWICH COMPOSITE BEAMS for STRUCTURAL APPLICATIONS

Module-6: Laminated Composites-II. Learning Unit-1: M6.1. M 6.1 Structural Mechanics of Laminates

ACDC. User Manual. Ver. 1.0

Tensile behaviour of anti-symmetric CFRP composite

A Study on the Tube of Integral Propeller Shaft for the Rear-wheel Drive Automobile Using Carbon Composite Fiber

COMPUTER AIDED DESIGN IN CASE OF THE LAMINATED COMPOSITE MATERIALS

Module III - Macro-mechanics of Lamina. Lecture 23. Macro-Mechanics of Lamina

An orthotropic damage model for crash simulation of composites

Analysis of Flexural Properties of Carbon Fiber Reinforced / E-Poxy Composite Material

FIXED BEAMS IN BENDING

Indentation Energy in Bending of Sandwich Beams with Composite Laminated Faces and Foam Core

BEAM DEFLECTION THE ELASTIC CURVE

SOME RESEARCH ON FINITE ELEMENT ANALYSIS OF COMPOSITE MATERIALS

5. What is the moment of inertia about the x - x axis of the rectangular beam shown?

ON THE NUMERICAL ANALYSIS OF COMPOSITE MATERIAL

Program: Recent Trends

ASPECTS CONCERNING TO THE MECHANICAL PROPERTIES OF THE GLASS / FLAX / EPOXY COMPOSITE MATERIAL

2 marks Questions and Answers

Project Name Structural Calculation for Feature Pressing

LOCAL BOND STRESS SLIP RELATIONS FOR FRP SHEETS-CONCRETE INTERFACES

Use Hooke s Law (as it applies in the uniaxial direction),

For more Stuffs Visit Owner: N.Rajeev. R07

As an example we consider the stacking and analysis of a 2-ply symmetric laminate. First we clear the Matlab space and close figures.

EE C247B / ME C218 INTRODUCTION TO MEMS DESIGN SPRING 2014 C. Nguyen PROBLEM SET #4

LAMINATION THEORY FOR THE STRENGTH OF FIBER COMPOSITE MATERIALS

TABLE OF CONTENTS. Mechanics of Composite Materials, Second Edition Autar K Kaw University of South Florida, Tampa, USA

THE MUTUAL EFFECTS OF SHEAR AND TRANSVERSE DAMAGE IN POLYMERIC COMPOSITES

CHEM-E2200: Polymer blends and composites Fibre architecture and principles of reinforcement

Strength of Materials Prof. Dr. Suraj Prakash Harsha Mechanical and Industrial Engineering Department Indian Institute of Technology, Roorkee

PERIYAR CENTENARY POLYTECHNIC COLLEGE PERIYAR NAGAR - VALLAM THANJAVUR. DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK

Chapter 5. Vibration Analysis. Workbench - Mechanical Introduction ANSYS, Inc. Proprietary 2009 ANSYS, Inc. All rights reserved.

Keywords: CFRP, compressive failure, kink-band, cohesive zone model. * Corresponding author

Massachusetts Institute of Technology Department of Aeronautics and Astronautics Cambridge, MA Problem Set 14

Lecture 16-17, Sandwich Panel Notes, 3.054

Nonlinear bending analysis of laminated composite stiffened plates

Non-conventional Glass fiber NCF composites with thermoset and thermoplastic matrices. F Talence, France Le Cheylard, France

MECE 3321: Mechanics of Solids Chapter 6

Passive Damping Characteristics of Carbon Epoxy Composite Plates

Composite Structural Mechanics using MATLAB

Dynamic Analysis of Laminated Composite Plate Structure with Square Cut-Out under Hygrothermal Load

A Numerical Study on Prediction of BFS in Composite Structures under Ballistic Impact

to introduce the principles of stability and elastic buckling in relation to overall buckling, local buckling

Basic and Special Design Concepts of CLT Elements loaded out-of-plane

[8] Bending and Shear Loading of Beams

IJSER 1. INTRODUCTION. M.Elhadary

Improving the Accuracy of Dynamic Vibration Fatigue Simulation

Laboratory 4 Bending Test of Materials

Metric (S.I. Units System) English (U.S. Units System) Method PHYSICAL

Getting Started with Composites Modeling and Analysis

KINK BAND FORMATION OF FIBER REINFORCED POLYMER (FRP)

Evaluation of Flexural Stiffness for RC Beams During Fire Events

Reliable Test Results

Chapter 1 General Introduction Instructor: Dr. Mürüde Çelikağ Office : CE Building Room CE230 and GE241

FLOATING NODE METHOD AND VIRTUAL CRACK CLOSURE TECHNIQUE FOR MODELING MATRIX CRACKING- DELAMINATION MIGRATION

Module 5: Laminate Theory Lecture 17: Laminate Constitutive Relations. The Lecture Contains: Laminate Constitutive Relations

Nonlinear Modeling of Fiber-Reinforced Elastomers and the Response of a Rubber Muscle Actuator

Influence of residual stresses in the structural behavior of. tubular columns and arches. Nuno Rocha Cima Gomes

DESIGN OF LAMINATES FOR IN-PLANE LOADING

Design of Beams (Unit - 8)

Theoretical Approach to Predict Transverse Impact Response of Variable-Stiffness Curved Composite Plates

Calibration and Experimental Validation of LS-DYNA Composite Material Models by Multi Objective Optimization Techniques

BI-STABLE COMPOSITE SHELLS

CHAPTER -6- BENDING Part -1-

AM11: Diagnostics for Measuring and Modelling Dispersion in Nanoparticulate Reinforced Polymers. Polymers: Multiscale Properties.

SECTION 23 - METRIC DESIGN INFORMATION. Table of Contents

PLY LEVEL UNCERTAINTY EFFECTS ON FAILURE OF COMPOSITE

Thermal buckling and post-buckling of laminated composite plates with. temperature dependent properties by an asymptotic numerical method

Materials: engineering, science, processing and design, 2nd edition Copyright (c)2010 Michael Ashby, Hugh Shercliff, David Cebon.

A copy can be downloaded for personal non-commercial research or study, without prior permission or charge

ri [11111 IlL DIRECTIONAL PROPERTIES Of GLASS-FABRIC-BASE PLASTIC LAMINATE PANELS Of SIZES THAT DO NOT IBUCICLE (P-Q1lAtVjr) No.

Passive Damping Characteristics of Carbon Epoxy Composite Plates

NUMERICAL VERIFICATION OF GEOTECHNICAL STRUCTURE IN UNFAVOURABLE GEOLOGICAL CONDITIONS CASE STUDY

MATERIAL PROPERTIES. Material Properties Must Be Evaluated By Laboratory or Field Tests 1.1 INTRODUCTION 1.2 ANISOTROPIC MATERIALS

Sensitivity Analysis with Correlated Variables

SIMPLIFIED METHOD FOR PREDICTING DEFORMATIONS OF RC FRAMES DURING FIRE EXPOSURE

Micro-meso draping modelling of non-crimp fabrics

FIS Specifications for Flex Poles (Edition May 2008) Original Text: German

THERMAL STRESS ANALYSIS OF A FIBER-EPOXY COMPOSITE MATERIAL

Effects of mesostructure on the in-plane properties of tufted carbon fabric composites

Transcription:

Statistical Optimization and Structural Analysis: Design of handmade custom Snowboards Benoit CAILLAUD 4th Workshop on Structural Analysis of Lightweight Structures Innsbruck, 02.06.2016 1

Agenda Introduction Materials & Structure, Geometry & Shape 1. Calibration of test feedback Elaboration of questionnaires Overview of first results 2. Correlation of test results with board parameters Direct Sensitivity Study and ranking of significant parameters Application: optimization of custom handmade snowboards 3. Optimization under Structural analysis Ranking of significant parameters according to certain target outputs Board parameters Analysis results Test results Conclusions 2

Materials & Structure Wood Composite reinforcements Layup Edges Thickness profile Input parameters: Sidewalls - Wood species combinations - Thickness profile - Reinforcement & Matrix types - Layup (orientation, thickness, stacking sequence) - Material properties (E Modulus {El Et Glt}, Poisson ratios) - Tensile, Compessive, Flexural Strength {σ e }, {σ r } - Density, Toughness, Stability UD Roving UD Lin fiber ±45 fabric Basalte UD Roving 3

Geometry & Shape Dimensions Sidecut shape Camber profile Inserts positions Input parameters: - L, L m, L contact - L nose, L tail, L camber - W nose, W waist, W tail - Stance - Setback - H nose, H tail, H camber - Curvatures: sidecut, camber, rockers Sidecut Radius [m] 40 30 20 10 0-800 -600-400 -200 0 200 400 600 800 4

Portfolio 5

Calibration of test feedback 25 output parameters including: - Board behaviour (discipline related) - Board aspect (graphics, weight) - Terrain conditions (weather, snow quality) 35 feedback results gathered over Winter 15/16 6

Calibration of test feedback I m gonna die I m loving it Boring A lot of fun! Very slippery Very grippy Too stiff Too soft 7

Calibration of test feedback Too Sinks short easily Floats Too easily long 8

Correlation of test results Direct Sensitivity Study: - Compute Correlation Coefficients between two sets of {Inputs} and {Outputs} determine which parameters are significant to which outputs 6 5 4 3 2 1 0 Nose float = f(taper) Nose float = f(bindings Setback) Nose float = f(nose Rocker) 0 5 10 15 20 Taper [mm] 6 5 4 3 2 1 0 0 10 20 30 40 50 Bindings Setback [mm] 6 5 4 3 2 1 0 0 20 40 60 Nose Rocker [mm] CC = 0.258 CC = 0.135 CC = 0.061 Slope = 46,6.10-3 Slope = 8,3.10-3 Slope = 4,3.10-3 - Quantify parameter influence (slope of fitted numerical model) compare effects of different parameters input parameters must be standardized to their practical variation range 9

"Overall Stiffness" feedback Dx [N.mm] Correlation of test results 6 "Overall stiffness" = f(dx) 5 4 3 2 1 CC = 0.584 0 2.0E+05 4.0E+05 6.0E+05 8.0E+05 1.0E+06 Average Bending Stiffness Dx [N.mm] «Too soft» «Too stiff» Feedback parameter «Global Stiffness» 10

Dx [N.mm] Dx [N.mm] Structural Analysis Optimization Sensitivity Study: computation of average bending Stiffnesses for different layups Stacking sequence (symmetric) Material Orientation Thickness (mean value) Fiberglass ±45 t 45 = 0,4mm Fiberglass 0 t 0 = 0,4mm Wood core 0 t core = 6,8mm Fiberglass 0 t 0 = 0,4mm Fiberglass ±45 t 45 = 0,4mm Input parameters 3 (t core, t 0, t 45 ) Variation interval ±15% Number of samples 2197 (all combinations) Theory of thin laminates, [ABD] -1 matrix Average bending stiffness D x [N.mm] D x = f(t c ) 1200000 1100000 1000000 900000 800000 700000 600000 500000 400000 5.0 6.0 7.0 8.0 Core thickness tc [mm] CC = 0.980 CC = 0.130 Slope = 2,6.10 D x = f(t 0 ) 5 1400000 1200000 1000000 800000 600000 400000 200000 Slope = 9,2.10 5 0 0.32 0.37 0.42 0.47 UD Fiberglass, layer thickness t0 [mm] 11

Dx [N.mm] Structural Analysis Optimization - Define optimization target parameter (Mass, Material Cost, Time ) - Assess variation of single parameters around the deterministic sample - Sort the parameters by influence ranking 900000 850000 Optimization of structural thickness according to output Mass [kg] 800000 750000 700000 650000 Deterministic sample 600000 2.8 2.85 2.9 2.95 3 3.05 3.1 M (0,35m²) [kg] Variation of CORE thickness only Variation of UD PLY thickness only Variation of 45 PLY thickness only 12

Conclusions Design of a custom snowboard: 1) Define the board specifications: for whom? for which activity? 2) Pick up the best fit among all existing shapes, based on rider profile and feedback results 3) Run sensitivity study with the chosen existing board as "mean value" 4) Optimization of geometrical and structural parameters using the study results: - sort significant input parameter by influence level (descending) - define priorities and «best compromise» Further steps: - Expand number of samples and feedback results - Structural analysis via FE modelization: consideration of field inputs and selected load cases - Qualification of material data - Consideration of physical inputs correlation - Fitting of nonlinear numerical models 13

Thanks! www.baguetteboards.com