Mechanically Efficient Cellular Microstructures in Plants. Lorna J. Gibson Materials Science & Engineering MIT

Similar documents
Lecture 16-17, Sandwich Panel Notes, 3.054

Wood structure Gibson, L. J., and M. F. Ashby. Cellular Solids: Structure and Properties. 2nd ed. Cambridge University Press, Figure courtesy of

Structural and torsional properties of the Trachycarpus fortunei palm petiole

Lecture 6, Wood notes, 3.054

STRENGTH OF WHEAT AND BARLEY STEMS AND DESIGN OF NEW BEAM/COLUMNS. Manisa, Turkey.

Lecture 4 Honeycombs Notes, 3.054

QUESTION BANK SEMESTER: III SUBJECT NAME: MECHANICS OF SOLIDS

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

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV

QUESTION BANK DEPARTMENT: CIVIL SEMESTER: III SUBJECT CODE: CE2201 SUBJECT NAME: MECHANICS OF SOLIDS UNIT 1- STRESS AND STRAIN PART A

UNIT-I STRESS, STRAIN. 1. A Member A B C D is subjected to loading as shown in fig determine the total elongation. Take E= 2 x10 5 N/mm 2

2012 MECHANICS OF SOLIDS

Lecture 7, Foams, 3.054

R13. II B. Tech I Semester Regular Examinations, Jan MECHANICS OF SOLIDS (Com. to ME, AME, AE, MTE) PART-A

SRI CHANDRASEKHARENDRA SARASWATHI VISWA MAHAVIDHYALAYA


Variation in Microstructure and Mechanical Properties of Tre Gai bamboo (Bambusa stenostachya) with Position in the Culm

3 Hours/100 Marks Seat No.

CIV 207 Winter For practice

Name :. Roll No. :... Invigilator s Signature :.. CS/B.TECH (CE-NEW)/SEM-3/CE-301/ SOLID MECHANICS

Question 1. Ignore bottom surface. Solution: Design variables: X = (R, H) Objective function: maximize volume, πr 2 H OR Minimize, f(x) = πr 2 H

Mechanics of Irregular Honeycomb Structures

CIVIL DEPARTMENT MECHANICS OF STRUCTURES- ASSIGNMENT NO 1. Brach: CE YEAR:

UNIT 1 STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS 1. Define stress. When an external force acts on a body, it undergoes deformation.

STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS

FINAL EXAMINATION. (CE130-2 Mechanics of Materials)

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

2. (a) Explain different types of wing structures. (b) Explain the advantages and disadvantages of different materials used for aircraft

Macroscopic Elastic Constitutive Relationship of Cast-in-Place Hollow-Core Slabs

2. Determine the deflection at C of the beam given in fig below. Use principal of virtual work. W L/2 B A L C

MAAE 2202 A. Come to the PASS workshop with your mock exam complete. During the workshop you can work with other students to review your work.

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each.

PES Institute of Technology

Downloaded from Downloaded from / 1

COURSE STE6289 Modern Materials and Computations (Moderne materialer og beregninger 7.5 stp.)

2. Rigid bar ABC supports a weight of W = 50 kn. Bar ABC is pinned at A and supported at B by rod (1). What is the axial force in rod (1)?

Mechanics of Inflatable Fabric Beams

= 50 ksi. The maximum beam deflection Δ max is not = R B. = 30 kips. Notes for Strength of Materials, ET 200

: APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4021 COURSE CATEGORY : A PERIODS/ WEEK : 5 PERIODS/ SEMESTER : 75 CREDIT : 5 TIME SCHEDULE

Materials and Shape. Part 1: Materials for efficient structure. A. K. M. B. Rashid Professor, Department of MME BUET, Dhaka. Learning Objectives

CE6306 STRENGTH OF MATERIALS TWO MARK QUESTIONS WITH ANSWERS ACADEMIC YEAR

Stress Analysis Lecture 4 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy

Mechanical Engineering Ph.D. Preliminary Qualifying Examination Solid Mechanics February 25, 2002

18.Define the term modulus of resilience. May/June Define Principal Stress. 20. Define Hydrostatic Pressure.

Chapter 3. Load and Stress Analysis

AERO 214. Lab II. Measurement of elastic moduli using bending of beams and torsion of bars

COURSE TITLE : APPLIED MECHANICS & STRENGTH OF MATERIALS COURSE CODE : 4017 COURSE CATEGORY : A PERIODS/WEEK : 6 PERIODS/ SEMESTER : 108 CREDITS : 5

By Dr. Mohammed Ramidh

Sample Question Paper

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each. Q.1 Find the force (in kn) in the member BH of the truss shown.

Johns Hopkins University What is Engineering? M. Karweit MATERIALS

ME Final Exam. PROBLEM NO. 4 Part A (2 points max.) M (x) y. z (neutral axis) beam cross-sec+on. 20 kip ft. 0.2 ft. 10 ft. 0.1 ft.

PURE BENDING. If a simply supported beam carries two point loads of 10 kn as shown in the following figure, pure bending occurs at segment BC.

MAHALAKSHMI ENGINEERING COLLEGE

COLUMNS: BUCKLING (DIFFERENT ENDS)

Advanced Structural Analysis EGF Section Properties and Bending

Critical Load columns buckling critical load

MITOCW watch?v=4zpqwirfsbk

NORMAL STRESS. The simplest form of stress is normal stress/direct stress, which is the stress perpendicular to the surface on which it acts.

Mechanics of Materials II. Chapter III. A review of the fundamental formulation of stress, strain, and deflection

Solution: The moment of inertia for the cross-section is: ANS: ANS: Problem 15.6 The material of the beam in Problem

Solution: The strain in the bar is: ANS: E =6.37 GPa Poison s ration for the material is:

ISHIK UNIVERSITY DEPARTMENT OF MECHATRONICS ENGINEERING

Stress Analysis Lecture 3 ME 276 Spring Dr./ Ahmed Mohamed Nagib Elmekawy

Unit 18 Other Issues In Buckling/Structural Instability

CHAPTER THREE SYMMETRIC BENDING OF CIRCLE PLATES

UNIT-I Introduction & Plane Stress and Plane Strain Analysis

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 10 Columns

Properties of Sections

STRENGTH OF MATERIALS-I. Unit-1. Simple stresses and strains

COURSE TITLE : THEORY OF STRUCTURES -I COURSE CODE : 3013 COURSE CATEGORY : B PERIODS/WEEK : 6 PERIODS/SEMESTER: 90 CREDITS : 6

Engineering Science OUTCOME 1 - TUTORIAL 4 COLUMNS

3. BEAMS: STRAIN, STRESS, DEFLECTIONS

1.050: Beam Elasticity (HW#9)

Homework No. 1 MAE/CE 459/559 John A. Gilbert, Ph.D. Fall 2004

External Pressure... Thermal Expansion in un-restrained pipeline... The critical (buckling) pressure is calculated as follows:

Symmetric Bending of Beams

LATERAL STABILITY OF BEAMS WITH ELASTIC END RESTRAINTS

The example of shafts; a) Rotating Machinery; Propeller shaft, Drive shaft b) Structural Systems; Landing gear strut, Flap drive mechanism

BME 207 Introduction to Biomechanics Spring 2017

ROTATING RING. Volume of small element = Rdθbt if weight density of ring = ρ weight of small element = ρrbtdθ. Figure 1 Rotating ring

GATE SOLUTIONS E N G I N E E R I N G

Problem d d d B C E D. 0.8d. Additional lecturebook examples 29 ME 323

EFFECTIVE SIMULATION APPROACH FOR STUDY OF CARBON NANOTUBE MECHANICAL PROPERTIES

Practice Final Examination. Please initial the statement below to show that you have read it

Design of Reinforced Concrete Structures (II)

GEOSYNTHETICS ENGINEERING: IN THEORY AND PRACTICE

EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 3 Torsion

MATERIALS. Why do things break? Why are some materials stronger than others? Why is steel tough? Why is glass brittle?

Mechanics of Materials MENG 270 Fall 2003 Exam 3 Time allowed: 90min. Q.1(a) Q.1 (b) Q.2 Q.3 Q.4 Total

Nomenclature. Length of the panel between the supports. Width of the panel between the supports/ width of the beam

MITOCW watch?v=wifaha1iav4

Members Subjected to Torsional Loads

NAME: Given Formulae: Law of Cosines: Law of Sines:

Chapter 5 Elastic Strain, Deflection, and Stability 1. Elastic Stress-Strain Relationship

ARTICLE A-8000 STRESSES IN PERFORATED FLAT PLATES

Outline. Organization. Stresses in Beams

Chapter 5 Torsion STRUCTURAL MECHANICS: CE203. Notes are based on Mechanics of Materials: by R. C. Hibbeler, 7th Edition, Pearson

UNIT- I Thin plate theory, Structural Instability:

Transcription:

Mechanically Efficient Cellular Microstructures in Plants Lorna J. Gibson Materials Science & Engineering MIT 1

Introduction Plants are typically loaded in bending by wind and in compression by self-weight Minimizing mass reduces metabolic cost to grow material Examine strategies used in plants to reduce mass 2

Introduction Wood: Uniform honeycomb-like structure Palm stem: Radial density gradient Plant stem: Cylindrical shell with compliant core Monocotyledon leaves: Sandwich structures 3

Wood: Honeycomb-Like Microstructure Cedar 4

Wood: Honeycomb Models E * E salong = ρ* ρ s Cell wall: Fiber Composite Model E * = ρ* E sacross ρ s 3 5

Wood in Bending: E 1/2 /ρ ( E * ) 1/2 ρ * ( = E s) 1/2 ρ s ρ s ρ * 1/2 Wood cell wall Stiffness performance index for wood in bending is similar to that for best engineering composites 6

Wood in Bending: σ f 2/3 /ρ ( * σ ) 2/3 f ρ * ( = σ ) 2/3 ys ρ s ρ s ρ * 1/3 Strength performance index for wood in bending is similar to that for best engng composites 7

Wood Tree in bending loaded as cantilever Radius decreases with distance away from the ground Further increases mechanical performance of the tree E = constant, r = r (z) 8

Palm Stem: Radial Density Gradient (Also Bamboo) 9

Palm Stem: A Different Strategy Stem has constant diameter: r = constant As palm grows taller, it increases the density of the material towards its periphery Cell wall thickness increases towards periphery of stem and towards the base of the stem E = E (r, z) Coconut Palm http://en.wikipedia.org/wiki/ Image:Palmtree_Curacao.jpg 10

Palm: Microstructure of Peripheral Stem Tissue Rich, 1987 6 μm 10 μm Kuo-Huang et al., 2004 Young Old 11

Palm Stem: Density Gradient Rich, PM (1987) Bot.Gazette 148, 42-50. 12

Palm Stem: Density at Breast Height Densities of common woods A single mature palm has a similar range of density as nearly all species of wood combined Rich, PM (1987) Bot.Gazette 148, 42-50. 13

Palm Stem: Density Gradient 14

Palm Stem: Mechanical Properties vs. Density Rich, PM (1987) Bot.Gazette 148, 42-50. 15

Density Gradient: Iriartea gigantea ρ = r r o n ρ max ( EI) gradient = Cπr o mn + 4 4 E = C ρ ρ max m = C r r o mn ( EI) gradient = ( EI) uniform 4 mn + 4 n + 2 2 m Iriartea palm: n = 2, m = 2.5, (EI) gradient /(EI) uniform = 2.5 Similar calculation for Welfia georgii, gives (EI) gradient /(EI) uniform = 1.6 16

Palm Stem: Bending Stress Distribution σ(y) = Eε = Eκ y σ(r,θ) = C r r o mn κr cosθ r mn+1 Iriartea gigantea: m = 2.5, n =2 σ r 6 17

Palm Stem: Bending Strength Distribution σ * ρ ρ max q r r o nq Iriartea gigantea: n = 2, q = 2 σ * r 4 Strength matches bending stress distribution 18

Plant Stems: Cylindrical Shells with Compliant Cores (Also in Animal Quills, Toucan Beak) 19

Plant Stems Milkweed Grassy stem 20

Milkweed Stem 21

Grassy Stem Hollow struts 22

Plant stems Circular tube cross-section Resists bending (wind loads) Maximize shape factor Φ= 4π I A 2 = a t Maximize a/t, but limited by local buckling and ovalization Plant stems have compliant core ( core-rind structure ) 23

Plant Stems: Bending Core resists ovalization and increases local buckling resistance 24

Plant Stems: Bending Local buckling occurs when normal stress in compressive side of cylinder equals critical stress for axisymmetric buckling under uniaxial stress Hollow cylinder: M lb = 0.939Eat 2 1 ν 2 Cylinder with compliant core: M lb = πea2 t 1 ν f δ 2 r, E core, a E shell t 25

Plant Stems Foam-like core can act like elastic foundation supporting outer shell, increasing local buckling moment, M lb, reducing buckling λ Hollow tube E c increasing 26

Plant Stems Hollow tube 27

Plant Stems Within the core stress decays as move radially inward, away from the shell Stresses less than 5% of maximum at a radial distance of 5λ cr Can remove inner core, leaving core thickness, c = 5λ cr 28

Plant Stems Species a/t Elastic foundation M lb /M eq c/λ cr Tall blue lettuce 59 Yes 1.37 3.81 Oat, rye grasses 50 Yes 1.26 3.81 Sedge grass, common barley 25 Yes 0.77 3.27 Core increases buckling resistance for high a/t 29

Monocotyledon Leaves: Sandwich Structures (Also in Skulls, Cuttlefish Bone, Horseshoe Crab Shell) 30

Monocotyledon Leaves: Sandwich Beams Iris Bulrush 31

Sandwich Structures: Leaves Sclerenchyma Parenchyma 0.5 mm Iris leaf 1mm Bulrush leaf 32

Sandwich Structures: Leaves Stipa gigantea (Giant feather grass) Lolium perenne (Rye grass) Black = sclerenchyma White = parenchyma Vincent, 1982,1991 33

Monocotyledon Leaves Fibers (sclerenchyma) along outer surface of leaves Foam-like cells (parenchyma) or ribs in core Acts like structural sandwich panel Increase in moment of inertia by separating stiff faces by a lightweight core Large surface area for photosynthesis 34

Sandwich Beam Deflection δ = δ b + δ s = B 1 Pl 3 + ( EI) eq B 2 Pl ( AG) eq Flexural rigidity: ( EI) eq E f btc2 2 Shear rigidity: ( AG) eq bcg c Cantilever: B 1 =3 B 2 = 1 35

Iris Leaves t = 30 μm c = 0.5 to 3.0 mm E f = 8.2 GPa G c =2 MPa Measured stiffnesses (N/mm): 0.66 0.54 0.41 0.25 Calculated stiffnesses (N/mm): 1.21 0.78 0.51 0.29 Calculated/measured: 1.83 1.44 1.24 1.16 36

Conclusion Wood Uniform honeycomb increases E 1/2 /ρ, σ f 2/3 /ρ Constant ρ, E, σ f, vary r(z) in tree Palm stem Radial density gradient Constant r, vary ρ(r), E(r), σ f (r) in palm stem Increases (EI) relative to uniform distribution of solid Stress distribution across radius matches strength distribution 37

Conclusion Plant stems Cylindrical shell with compliant core Increases buckling resistance over equivalent hollow circular tube for large a/t Monocotyledon leaves Sandwich structure, efficient in bending Leaves provide own structural support as well as area for photosynthesis Rectangular cross-section maximizes surface area for photosynthesis 38

Acknowledgements Mike Ashby, Ken Easterling, Hugh Shercliff Gebran Karam, Phoebe Cheng, Ulrike Wegst, Ros Olive, Tessa Shercliff Justin Breucop, Don Galler, Beth Beighlie National Science Foundation Matoula S. Salapatas Professorship at MIT 39

Image References Connor S (1994) New England Natives: A celebration of people and trees. Harvard University Press. Dinwoodie J (1981)Timber: Its nature and behaviour. Van Nostrand Reinhold. Rich PM (1987) Mechanical structure of the stem of arborescent palms. Bot. Gazette 148, 42. Rich PM (1987) Developmental anatomy of the stem of Welfia Georgii, Iriartea Gigantea and other arborescent palms: Implications for mechanical support. Am. J. Botany 74, 792. 40