What Is the Young's Modulus of Silicon?
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10-1 CHAPTER 10 DEFORMATION 10.1 Stress-Strain Diagrams And
EN380 Naval Materials Science and Engineering Course Notes, U.S. Naval Academy CHAPTER 10 DEFORMATION 10.1 Stress-Strain Diagrams and Material Behavior 10.2 Material Characteristics 10.3 Elastic-Plastic Response of Metals 10.4 True stress and strain measures 10.5 Yielding of a Ductile Metal under a General Stress State - Mises Yield Condition. 10.6 Maximum shear stress condition 10.7 Creep Consider the bar in figure 1 subjected to a simple tension loading F. Figure 1: Bar in Tension Engineering Stress () is the quotient of load (F) and area (A). The units of stress are normally pounds per square inch (psi). = F A where: is the stress (psi) F is the force that is loading the object (lb) A is the cross sectional area of the object (in2) When stress is applied to a material, the material will deform. Elongation is defined as the difference between loaded and unloaded length ∆푙 = L - Lo where: ∆푙 is the elongation (ft) L is the loaded length of the cable (ft) Lo is the unloaded (original) length of the cable (ft) 10-1 EN380 Naval Materials Science and Engineering Course Notes, U.S. Naval Academy Strain is the concept used to compare the elongation of a material to its original, undeformed length. Strain () is the quotient of elongation (e) and original length (L0). Engineering Strain has no units but is often given the units of in/in or ft/ft. ∆푙 휀 = 퐿 where: is the strain in the cable (ft/ft) ∆푙 is the elongation (ft) Lo is the unloaded (original) length of the cable (ft) Example Find the strain in a 75 foot cable experiencing an elongation of one inch. -
Static Analysis of Isotropic, Orthotropic and Functionally Graded Material Beams
Journal of Multidisciplinary Engineering Science and Technology (JMEST) ISSN: 2458-9403 Vol. 3 Issue 5, May - 2016 Static analysis of isotropic, orthotropic and functionally graded material beams Waleed M. Soliman M. Adnan Elshafei M. A. Kamel Dep. of Aeronautical Engineering Dep. of Aeronautical Engineering Dep. of Aeronautical Engineering Military Technical College Military Technical College Military Technical College Cairo, Egypt Cairo, Egypt Cairo, Egypt [email protected] [email protected] [email protected] Abstract—This paper presents static analysis of degrees of freedom for each lamina, and it can be isotropic, orthotropic and Functionally Graded used for long and short beams, this laminated finite Materials (FGMs) beams using a Finite Element element model gives good results for both stresses and deflections when compared with other solutions. Method (FEM). Ansys Workbench15 has been used to build up several models to simulate In 1993 Lidstrom [2] have used the total potential different types of beams with different boundary energy formulation to analyze equilibrium for a conditions, all beams have been subjected to both moderate deflection 3-D beam element, the condensed two-node element reduced the size of the of uniformly distributed and transversal point problem, compared with the three-node element, but loads within the experience of Timoshenko Beam increased the computing time. The condensed two- Theory and First order Shear Deformation Theory. node system was less numerically stable than the The material properties are assumed to be three-node system. Because of this fact, it was not temperature-independent, and are graded in the possible to evaluate the third and fourth-order thickness direction according to a simple power differentials of the strain energy function, and thus not law distribution of the volume fractions of the possible to determine the types of criticality constituents. -
Constitutive Relations: Transverse Isotropy and Isotropy
Objectives_template Module 3: 3D Constitutive Equations Lecture 11: Constitutive Relations: Transverse Isotropy and Isotropy The Lecture Contains: Transverse Isotropy Isotropic Bodies Homework References file:///D|/Web%20Course%20(Ganesh%20Rana)/Dr.%20Mohite/CompositeMaterials/lecture11/11_1.htm[8/18/2014 12:10:09 PM] Objectives_template Module 3: 3D Constitutive Equations Lecture 11: Constitutive relations: Transverse isotropy and isotropy Transverse Isotropy: Introduction: In this lecture, we are going to see some more simplifications of constitutive equation and develop the relation for isotropic materials. First we will see the development of transverse isotropy and then we will reduce from it to isotropy. First Approach: Invariance Approach This is obtained from an orthotropic material. Here, we develop the constitutive relation for a material with transverse isotropy in x2-x3 plane (this is used in lamina/laminae/laminate modeling). This is obtained with the following form of the change of axes. (3.30) Now, we have Figure 3.6: State of stress (a) in x1, x2, x3 system (b) with x1-x2 and x1-x3 planes of symmetry From this, the strains in transformed coordinate system are given as: file:///D|/Web%20Course%20(Ganesh%20Rana)/Dr.%20Mohite/CompositeMaterials/lecture11/11_2.htm[8/18/2014 12:10:09 PM] Objectives_template (3.31) Here, it is to be noted that the shear strains are the tensorial shear strain terms. For any angle α, (3.32) and therefore, W must reduce to the form (3.33) Then, for W to be invariant we must have Now, let us write the left hand side of the above equation using the matrix as given in Equation (3.26) and engineering shear strains. -
Life Cycle Analysis of High-Performance Monocrystalline Silicon Photovoltaic Systems: Energy Payback Times and Net Energy Production Value
27th European Photovoltaic Solar Energy Conference and Exhibition LIFE CYCLE ANALYSIS OF HIGH-PERFORMANCE MONOCRYSTALLINE SILICON PHOTOVOLTAIC SYSTEMS: ENERGY PAYBACK TIMES AND NET ENERGY PRODUCTION VALUE Vasilis Fthenakis1,2, Rick Betita2, Mark Shields3, Rob Vinje3, Julie Blunden3 1 Brookhaven National Laboratory, Upton, NY, USA, tel. 631-344-2830, fax. 631-344-3957, [email protected] 2Center for Life Cycle Analysis, Columbia University, New York, NY 10027, USA 3SunPower Corporation, San Jose, CA, USA ABSTRACT: This paper summarizes a comprehensive life cycle analysis based on actual process data from the manufacturing of Sunpower 20.1% efficient modules in the Philippines and other countries. Higher efficiencies are produced by innovative cell designs and material and energy inventories that are different from those in the production of average crystalline silicon panels. On the other hand, higher efficiencies result to lower system environmental footprints as the system area on a kW basis is smaller. It was found that high efficiencies result to a net gain in environmental metrics (i.e., Energy Payback Times, GHG emissions) in comparison to average efficiency c-Si modules. The EPBT for the Sunpower modules produced in the Philippines and installed in average US or South European insolation is only 1.4 years, whereas the lowest EPBT from average efficiency c-Si systems is ~1.7 yrs. To capture the advantage of high performance systems beyond their Energy Payback Times, we introduced the metric of Net Energy Production Value (NEPV), which shows the solar electricity production after the system has “paid-off” the energy used in its life-cycle. The SunPower modules are shown to produce 45% more electricity than average efficiency (i.e., 14%) c-Si PV modules. -
Orthotropic Material Homogenization of Composite Materials Including Damping
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Lirias Orthotropic material homogenization of composite materials including damping A. Nateghia,e, A. Rezaeia,e,, E. Deckersa,d, S. Jonckheerea,b,d, C. Claeysa,d, B. Pluymersa,d, W. Van Paepegemc, W. Desmeta,d a KU Leuven, Department of Mechanical Engineering, Celestijnenlaan 300B box 2420, 3001 Heverlee, Belgium. E-mail: [email protected]. b Siemens Industry Software NV, Digital Factory, Product Lifecycle Management – Simulation and Test Solutions, Interleuvenlaan 68, B-3001 Leuven, Belgium. c Ghent University, Department of Materials Science & Engineering, Technologiepark-Zwijnaarde 903, 9052 Zwijnaarde, Belgium. d Member of Flanders Make. e SIM vzw, Technologiepark Zwijnaarde 935, B-9052 Ghent, Belgium. Introduction In the multiscale analysis of composite materials obtaining the effective equivalent material properties of the composite from the properties of its constituents is an important bridge between different scales. Although, a variety of homogenization methods are already in use, there is still a need for further development of novel approaches which can deal with complexities such as frequency dependency of material properties; which is specially of importance when dealing with damped structures. Time-domain methods Frequency-domain method Material homogenization is performed in two separate steps: Wave dispersion based homogenization is performed to a static step and a dynamic one. provide homogenized damping and material -
2.1.5 Stress-Strain Relation for Anisotropic Materials
,/... + -:\ 2.1.5Stress-strain Relation for AnisotropicMaterials The generalizedHook's law relatingthe stressesto strainscan be writtenin the form U2, 13,30-32]: o,=C,,€, (i,i =1,2,.........,6) Where: o, - Stress('ompttnents C,, - Elasticity matrix e,-Straincomponents The material properties (elasticity matrix, Cr) has thirty-six constants,stress-strain relations in the materialcoordinates are: [30] O1 LI CT6 a, l O2 03_ a, -t ....(2-6) T23 1/ )1 T32 1/1l 'Vt) Tt2 C16 c66 I The relations in equation (3-6) are referred to as characterizing anisotropicmaterials since there are no planes of symmetry for the materialproperties. An alternativename for suchanisotropic material is a triclinic material. If there is one plane of material property symmetry,the stress- strainrelations reduce to: -'+1-/ ) o1 c| ct2 ct3 0 0 crc €l o2 c12 c22 c23 0 0 c26 a: ct3 C23 ci3 0 0 c36 o-\ o3 ....(2-7) 723 000cqqc450 y)1 T3l 000c4sc5s0 Y3l T1a ct6 c26 c36 0 0 c66 1/t) Where the plane of symmetryis z:0. Such a material is termed monoclinicwhich containstfirfen independentelastic constants. If there are two brthogonalplanes of material property symmetry for a material,symmetry will existrelative to a third mutuallyorthogonal plane. The stress-strainrelations in coordinatesaligned with principal material directionswhich are parallel to the intersectionsof the three orthogonalplanes of materialsymmetry, are'. Ol ctl ct2ctl000 tl O2 Ct2 c22c23000 a./ o3 ct3 c23c33000 * o-\ ....(2-8) T23 0 00c4400 y)1 yll 731 0 000css0 712 0 0000cr'e 1/1) 'lt"' -' , :t i' ,/ Suchmaterial is calledorthotropic material.,There is no interaction betweennormal StreSSeS ot r 02, 03) andanisotropic materials. -
Lecture 13: Earth Materials
Earth Materials Lecture 13 Earth Materials GNH7/GG09/GEOL4002 EARTHQUAKE SEISMOLOGY AND EARTHQUAKE HAZARD Hooke’s law of elasticity Force Extension = E × Area Length Hooke’s law σn = E εn where E is material constant, the Young’s Modulus Units are force/area – N/m2 or Pa Robert Hooke (1635-1703) was a virtuoso scientist contributing to geology, σ = C ε palaeontology, biology as well as mechanics ij ijkl kl ß Constitutive equations These are relationships between forces and deformation in a continuum, which define the material behaviour. GNH7/GG09/GEOL4002 EARTHQUAKE SEISMOLOGY AND EARTHQUAKE HAZARD Shear modulus and bulk modulus Young’s or stiffness modulus: σ n = Eε n Shear or rigidity modulus: σ S = Gε S = µε s Bulk modulus (1/compressibility): Mt Shasta andesite − P = Kεv Can write the bulk modulus in terms of the Lamé parameters λ, µ: K = λ + 2µ/3 and write Hooke’s law as: σ = (λ +2µ) ε GNH7/GG09/GEOL4002 EARTHQUAKE SEISMOLOGY AND EARTHQUAKE HAZARD Young’s Modulus or stiffness modulus Young’s Modulus or stiffness modulus: σ n = Eε n Interatomic force Interatomic distance GNH7/GG09/GEOL4002 EARTHQUAKE SEISMOLOGY AND EARTHQUAKE HAZARD Shear Modulus or rigidity modulus Shear modulus or stiffness modulus: σ s = Gε s Interatomic force Interatomic distance GNH7/GG09/GEOL4002 EARTHQUAKE SEISMOLOGY AND EARTHQUAKE HAZARD Hooke’s Law σij and εkl are second-rank tensors so Cijkl is a fourth-rank tensor. For a general, anisotropic material there are 21 independent elastic moduli. In the isotropic case this tensor reduces to just two independent elastic constants, λ and µ. -
New Challenges and Possibilities for Silicon Based Solar Cells
1 New challenges and possibilities for silicon based solar cells Marisa Di Sabatino Dept of Materials Science and Engineering NTNU 2 Outline -What is a solar cell? -How does it work? -Silicon based solar cells manufacturing -Challenges and Possibilities -Concluding remarks 3 What is a solar cell? • It is a device that converts the energy of the sunlight directly into electricity. CB PHOTON Eph=hc/λ VB Electron-hole pair 4 How does a solar cell work? 5 How does a solar cell work? Current Semiconductor Eg + - P-n junction Metallic contacts Turid Worren Reenaas 6 How does a solar cell work? - Charge generation (electron-hole pairs) - Charge separation (electric field) - Charge transport 7 - Charge generation (electron-hole pairs) - Charge separation (electric field) - Charge transport Eph>>Eg Eph<<Eg Eph>Eg Eg CB Eph VB 8 - Charge generation (electron-hole pairs) - Charge separation (electric field) - Charge transport p-type C - - - - Fermi level - + + + + + n-type n-p junction v + - Electric field 9 - Charge generation (electron-hole pairs) - Charge separation (electric field) - Charge transport Back and front side of a silicon solar cell 10 Semiconductors Materials for solar cells 11 Why Silicon? Silicon: abundant, cheap, well-known technology 12 Silicon solar cell value chain 13 Silicon solar cells value chain From sand to solar cells… Raw Materials Efficiency Crystallization Isc, Voc, FF Feedstock Solar cell process Photo: Melinda Gaal 14 Multicrystalline silicon solar cells Directional solidification 15 Monocrystalline silicon solar cells Czochralski process 16 Crystallization methods for PV silicon • Multicrystalline silicon ingots: – Lower cost than monocrystalline – More defects (dislocations and impurities) • Monocrystalline silicon ingots: – Higher cost and lower yield – Oxygen related defects – Structure loss 17 Czochralski PV single crystal growth • Dominating process for single crystals • Both p (B-doped) and n (P-doped) type crystals • Growth rate 60 mm/h Challenges: •Productivity low due to slow growth, long cycle time.. -
15Th Workshop on Crystalline Silicon Solar Cells and Modules: Materials and Processes
A national laboratory of the U.S. Department of Energy Office of Energy Efficiency & Renewable Energy National Renewable Energy Laboratory Innovation for Our Energy Future th Proceedings 15 Workshop on Crystalline NREL/BK-520-38573 Silicon Solar Cells and Modules: November 2005 Materials and Processes Extended Abstracts and Papers Workshop Chairman/Editor: B.L. Sopori Program Committee: M. Al-Jassim, J. Kalejs, J. Rand, T. Saitoh, R. Sinton, M. Stavola, R. Swanson, T. Tan, E. Weber, J. Werner, and B. Sopori Vail Cascade Resort Vail, Colorado August 7–10, 2005 NREL is operated by Midwest Research Institute ● Battelle Contract No. DE-AC36-99-GO10337 th Proceedings 15 Workshop on Crystalline NREL/BK-520-38573 Silicon Solar Cells and Modules: November 2005 Materials and Processes Extended Abstracts and Papers Workshop Chairman/Editor: B.L. Sopori Program Committee: M. Al-Jassim, J. Kalejs, J. Rand, T. Saitoh, R. Sinton, M. Stavola, R. Swanson, T. Tan, E. Weber, J. Werner, and B. Sopori Vail Cascade Resort Vail, Colorado August 7–10, 2005 Prepared under Task No. WO97G400 National Renewable Energy Laboratory 1617 Cole Boulevard, Golden, Colorado 80401-3393 303-275-3000 • www.nrel.gov Operated for the U.S. Department of Energy Office of Energy Efficiency and Renewable Energy by Midwest Research Institute • Battelle Contract No. DE-AC36-99-GO10337 NOTICE This report was prepared as an account of work sponsored by an agency of the United States government. Neither the United States government nor any agency thereof, nor any of their employees, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or `process disclosed, or represents that its use would not infringe privately owned rights. -
Efficient Hydraulic Fluids Compressibility Is Still One of the Most Critically Important Factors
WORLDWIDE R. David Whitby Efficient hydraulic fluids Compressibility is still one of the most critically important factors. ydraulic fluids transmit power as a hydraulic system con- while phosphate and vegetable-oil esters have compressibilities H verts mechanical energy into fluid energy and subsequently similar to that of water. Polyalphaolefins are more compressible to mechanical work. To achieve this conversion efficiently, hydrau- than mineral oils. Water-glycol fluids are intermediate between lic fluids need to be relatively incompressible. Hydraulic fluids mineral oils and water. must also minimize wear, reduce friction, provide cooling and pre- Mineral oils are relatively incompressible, but volume reduc- vent rust and corrosion, be compatible with system components tions can be approximately 0.5% for pressures ranging from 6,900 and help keep the system free of deposits. kPa (1,000 psi) up to 27,600 kPa (4,000 psi). Compressibility in- Compressibility measures the rela- creases with pressure and temperature tive change in volume of a fluid or solid and has significant effects on high-pres- as a response to a change in pressure and sure fluid systems. Hydraulic oils typi- is the reciprocal of the volume-elastic cally contain 6% to 10% of dissolved air, modulus or bulk modulus of elasticity. which has no measurable effect on bulk Bulk modulus defines the pressure in- modulus provided it stays in solution. crease needed to cause a given relative Bulk modulus is an inherent property decrease in volume. of the hydraulic fluid and, therefore, is The bulk modulus of a fluid is nonlin- an inherent inefficiency of the hydraulic ear. -
Crack Tip Elements and the J Integral
EN234: Computational methods in Structural and Solid Mechanics Homework 3: Crack tip elements and the J-integral Due Wed Oct 7, 2015 School of Engineering Brown University The purpose of this homework is to help understand how to handle element interpolation functions and integration schemes in more detail, as well as to explore some applications of FEA to fracture mechanics. In this homework you will solve a simple linear elastic fracture mechanics problem. You might find it helpful to review some of the basic ideas and terminology associated with linear elastic fracture mechanics here (in particular, recall the definitions of stress intensity factor and the nature of crack-tip fields in elastic solids). Also check the relations between energy release rate and stress intensities, and the background on the J integral here. 1. One of the challenges in using finite elements to solve a problem with cracks is that the stress field at a crack tip is singular. Standard finite element interpolation functions are designed so that stresses remain finite a everywhere in the element. Various types of special b c ‘crack tip’ elements have been designed that 3L/4 incorporate the singularity. One way to produce a L/4 singularity (the method used in ABAQUS) is to mesh L the region just near the crack tip with 8 noded elements, with a special arrangement of nodal points: (i) Three of the nodes (nodes 1,4 and 8 in the figure) are connected together, and (ii) the mid-side nodes 2 and 7 are moved to the quarter-point location on the element side. -
Elastic Properties of Fe−C and Fe−N Martensites
Elastic properties of Fe−C and Fe−N martensites SOUISSI Maaouia a, b and NUMAKURA Hiroshi a, b * a Department of Materials Science, Osaka Prefecture University, Naka-ku, Sakai 599-8531, Japan b JST-CREST, Gobancho 7, Chiyoda-ku, Tokyo 102-0076, Japan * Corresponding author. E-mail: [email protected] Postal address: Department of Materials Science, Graduate School of Engineering, Osaka Prefecture University, Gakuen-cho 1-1, Naka-ku, Sakai 599-8531, Japan Telephone: +81 72 254 9310 Fax: +81 72 254 9912 1 / 40 SYNOPSIS Single-crystal elastic constants of bcc iron and bct Fe–C and Fe–N alloys (martensites) have been evaluated by ab initio calculations based on the density-functional theory. The energy of a strained crystal has been computed using the supercell method at several values of the strain intensity, and the stiffness coefficient has been determined from the slope of the energy versus square-of-strain relation. Some of the third-order elastic constants have also been evaluated. The absolute magnitudes of the calculated values for bcc iron are in fair agreement with experiment, including the third-order constants, although the computed elastic anisotropy is much weaker than measured. The tetragonally distorted dilute Fe–C and Fe–N alloys exhibit lower stiffness than bcc iron, particularly in the tensor component C33, while the elastic anisotropy is virtually the same. Average values of elastic moduli for polycrystalline aggregates are also computed. Young’s modulus and the rigidity modulus, as well as the bulk modulus, are decreased by about 10 % by the addition of C or N to 3.7 atomic per cent, which agrees with the experimental data for Fe–C martensite.