Out life 30 days at 70 F (21 C) Shelf life 6 months at 40 F (4 C) 12 months at 0 F (-18 C)
|
|
|
- Jocelyn Watson
- 6 years ago
- Views:
Transcription
1 F ( C) High T g Epoxy Resin System Typical applications General aviation Aerospace Industrial Sporting goods Out life 30 days at 70 F (21 C) Shelf life 6 months at 40 F (4 C) 12 months at 0 F (-18 C) Description 4708 is a 250 F (121 C) to 300 F (149 C) cure, high T g, controlled flow epoxy resin system specifically designed for out of autoclave processing. It provides versatile processing, excellent mechanical properties, and long out time significantly surpasses the performance of traditional 250 F (121 C) cure resin systems with its high toughness and impact resistance. Benefits/features Good dry and T g performance Excellent mechanical properties Vacuum bag and autoclave curable Application The elevated T g and excellent mechanical properties make 4708 an ideal product for general aviation, aerospace and industrial markets where products are required to retain their mechanical properties under demanding temperatures. Due to its exceptionally high T g, it is particularly suited for applications where hot/ performance is required can be supplied as a matrix for most commercially available fibers (carbon, quartz, aramid, S-glass, E-glass, etc.) in both woven form (designated as NB) as well as unidirectional tape (designated as NCT). Woven fabrics are available in standard commercial widths up to 60 inches (1.5 m). Unitape widths up to 39 inches (1 m) are available in standard fiber weights ranging from gsm ( psf). Recommended processing conditions 4708 can be cured at temperatures from 250 F to 300 F (121 C to 149 C) depending on part size and complexity. It was specifically designed for vacuum processing but may be cured in an autoclave. Vacuum cure cycle Cure cycle: Apply full vacuum, hold at RT for a minimum of 4 hours. Heat from RT to 265±10 F at 5 F/min (130±5.5 C at 2.8 C/min). When temperature reaches 255 F (124 C), hold at temperature for 2 hours. Cool to below 140 F (60 C). Thicker parts may need to use step cure to reduce the possibility of an exotherm. Please contact MRCFAC s technical service for more information Mitsubishi Chemical Carbon Fiber and Composites, Inc. All rights reserved Page 1 of 6
2 Neat resin [values are average and do not constitute a specification] Property Value Gel 275 F (135 C), minutes 4 7 Specific gravity 1.25 Dry T g (DMA, E ), C ( F) 145 (293) Wet T g (DMA, E ), C ( F)* 120 (248) Tensile strength, ksi (MPa) 9.0 (62) Tensile modulus, Msi (GPa) 0.47 (3.2) Tensile strain, % 2.4 Poisson s ratio 0.38 Compressive yield strength, ksi (MPa) 19.1 (131) Compressive yield modulus, Msi (GPa) 0.45 (3.1) Compressive ultimate strength, ksi (MPa) 38.9 (268) *14 days, 160 F water immersion Mechanical data [values are average and do not constitute a specification] MR60H Uni Carbon, 36%RC, vacuum bag cured, 120min at 265 F, norm. to 60%FV Property Test method -65 F (-53 C) RT 225 F (107 C) 401 (2760) 417 (2870) - 0 Tensile modulus, Msi (GPa) 23.6 (162) 24.5 (168) (43.1) 5.90 (40.6) 90 Tensile modulus, Msi (GPa) 1.28 (8.82) 1.15 (7.93) 1.19 ( (1710) 228 (1570) 189 (1300) 0 Compressive modulus, Msi (GPa) ASTM 20.9 (144) 21.9 (151) 20.7 (142) 9 D695mod 31.9 (220) 23.9 (164) - 90 Compressive modulus, Msi (GPa) 1.39 (9.58) 1.23 (8.48) (1570) 169 (1160) 0 Flexural modulus, Msi (GPa) (154) 22.6 (155) (94.4) 9.50 (65.5) * ±45 In-plane shear strength, ksi (MPa) 8.88 (61.2) 8.25 (56.8) - SACMA 5R-94 * ±45 In-plane shear modulus, Msi (GPa) 0.64 (4.4) (5.06) - 0 Short beam shear strength, ksi (MPa) SACMA 8R (86.8) 12.7 (87.5) 8.90 (61.3) Open hole tensile strength, ksi (MPa) 66.1 (455) 76.3 (526) - ASTM D5766 Open hole tensile modulus, Msi (GPa) (50.3) - Open hole compressive strength, ksi (MPa) ASTM D (270) - Compressive strength after impact, ksi (MPa) strain ASTM D7136 ASTM D (191) Mitsubishi Chemical Carbon Fiber and Composites, Inc. All rights reserved Page 2 of 6
3 MR60H Uni Carbon, 36%RC, vacuum bag cured, 120min at 265 F, norm. to 60%FV Property Test method 180 F (82 C) 180 F (82 C) * 437 (3010) 433 (2980) 0 Tensile modulus, Msi (GPa) 24.3 (167) 24.1 (166) (25.0) 90 Tensile modulus, Msi (GPa) (5.96) 200 (1370) 181 (1240) 0 Compressive modulus, Msi (GPa) 20.9 (144) 21.3 (146) ASTM D695mod (93.7) 90 Compressive modulus, Msi (GPa) (6.96) 184 (1260) 165 (1130) 0 Flexural modulus, Msi (GPa) 21.5 (148) 21.9 (151) (55.8) ** ±45 In-plane shear strength, ksi (MPa) 6.96 (48.0) 4.74 (32.6) SACMA 5R-94 ** ±45 In-plane shear modulus, Msi (GPa) (3.03) (2.48) 0 Short beam shear strength, ksi (MPa) SACMA 8R (63.8) 7.66 (52.8) Open hole tensile strength, ksi (MPa) 82.8 (571) 77.0 (531) ASTM D5766 Open hole tensile modulus, Msi (GPa) 7.55 (52.0) 7.40 (51.0) Open hole compressive strength, ksi (MPa) ASTM D (262) 33.6 (231) * 14 days, 160 F water immersion strain HS40 Uni Carbon, 145gsm, 35%RC, autoclave cured, 80 psi, 90min. at 275 F, norm. to 60%FV 345 (2370) 0 Tensile modulus, Msi (GPa) 37.3 (257) Poisson s ratio (1.57) 186 (1280) ASTM D695mod 0 Compressive modulus, Msi (GPa) 36.8 (253) 212 (1460) 0 Flexural modulus, Msi (GPa) 32.9 (226) 0 Short beam shear strength, ksi (MPa) ASTM D (86) 2015 Mitsubishi Chemical Carbon Fiber and Composites, Inc. All rights reserved Page 3 of 6
4 TR30S 3KPW Carbon fabric, 42%RC, autoclave cured, 80 psi, 90min. at 265 F, norm. to 60%FV 111 (765) 0 Tensile modulus, Msi (GPa) 9.6 (66) 106 (731) ASTM D695mod 0 Compressive modulus, Msi (GPa) 8.8 (60) 136 (937) 0 Flexural modulus, Msi (GPa) 8.8 (60) 0 Short beam shear strength, ksi (MPa) ASTM D (66) AS-4C 3K 8HS Carbon fabric, 40%RC, vacuum bag cured, 120min. at 265 F, norm. to 60%FV 225 F (107 C) 180 F (82 C) 200 F (93 C) 118 (813) 100 (689) 100 (689) - 0 Tensile modulus, Msi (GPa) 9.1 (62) 8.9 (61) 9.1 (62) - ASTM D695mod 103 (710) 75 (510) 74 (510) 65 (440) 140 (965) 92 (630) 89 (610) - 0 Flexural modulus, Msi (GPa) 8.2 (57) 7.4 (51) 7.5 (52) - 0 Short beam shear strength, ksi (MPa) SACMA 8R (68) 6.1 (42) 6.4 (44) 5.5 (37) 7781 E-glass fabric, 38% RC, vacuum bag cured, 3 F/min., 120min. at 265 F, norm. to 60%FV 225 F (107 C) 180 F (82 C) 200 F (93 C) ASTM D (696) 82 (565) 58 (400) - 0 Tensile modulus, Msi (GPa) Type II 4.7 (32) 5.1 (35) 4.7 (32) - ASTM 115 (793) 84 (579) 72 (496) 66 (455) 0 Compressive modulus, Msi (GPa) D695mod 5.0 (34) (34) (938) 99 (683) 80 (552) 74 (510) 0 Flexural modulus, Msi (GPa) 4.6 (32) 4.3 (30) 4.3 (30) 4.2 (29) 0 Short beam shear strength, ksi (MPa) SACMA 8R (18) 8.8 (12) 5.7 (7.7) 4.5 (6.1) 2015 Mitsubishi Chemical Carbon Fiber and Composites, Inc. All rights reserved Page 4 of 6
5 Viscosity profile TA - AR2000 parallel plate rheometer Time (min.) R R E5 Newport 4708 Viscosity vs Time n * ( p o is e ) poise, 128 C 50 poise, 121 C 60 poise, 115 C 100 poise, 107 C time (min) Gel curve 1 C/min 2 C/min 3 C/min 5 C/min 30 Gel time vs. temperature Temperature ( F) 2015 Mitsubishi Chemical Carbon Fiber and Composites, Inc. All rights reserved Page 5 of 6
6 Recommended bagging assembly 2015 Mitsubishi Chemical Carbon Fiber and Composites, Inc. All rights reserved Page 6 of 6
F ( C) Cure Epoxy Resin System. Out life 30 days at 70 F (21 C)
301 250-300 F (121-149 C) Cure Epoxy Resin System Typical applications Sporting goods Marine Medical Industrial manufacturing Benefits/features Excellent mechanical properties Moderate tack Good toughness
F ( C) Cure Epoxy Resin System. Out life 30 days at 70 F (21 C)
301 250-300 F (120-150 C) Cure Epoxy Resin System Typical applications Sporting goods Marine Medical Industrial manufacturing Out life 30 days at 70 F (21 C) Shelf life 6 months at 40 F (4 C) 12 months
2510 PREPREG SYSTEM. Industry Database FAA approved design allowable values (AGATE methodology), results in a low cost one-batch equivalency.
PREPREG SYSTEM The 251 prepreg system is specifically formulated for out-of-autoclave (OOA) processing of aerospace primary structures. This prepreg system has excellent all-around structural properties
2510 PREPREG SYSTEM. Industry Database FAA approved design allowable values (AGATE methodology), results in a low cost one-batch equivalency.
PREPREG SYSTEM The 251 prepreg system is specifically formulated for out-of-autoclave (OOA) processing of aerospace primary structures. This prepreg system has excellent all-around structural properties
3900 PREPREG SYSTEM. Mechanically Stable Mechanical working life of product is over 40 days, allowing for lay-up of large parts.
PREPREG SYSTEM -series prepregs are highly-toughened 350 F (177 C) cure systems. It is available in a variety of configurations, including unidirectional tape for manual or automated tape laying applications,
3900 PREPREG SYSTEM. Mechanically Stable Mechanical working life of product is over 40 days, allowing for lay-up of large parts.
PREPREG SYSTEM 3900-series prepregs are highly-toughened 350 F (177 C) cure systems. It is available in a variety of configurations, including unidirectional tape for manual or automated tape laying applications,
3960 PREPREG SYSTEM. Flexible Processing Prepreg can be suitably processed in either AFP or hand lay-up methodologies.
396 PREPREG SYSTEM Toray s nextgeneration #396 prepreg system demonstrates the next leap in performance of aerospace materials. Complementary pairing of the #396 resin system with stateoftheart T11G carbon
HexPly F655 Resin Systems for Advanced Composites
HexPly F655 Resin Systems for Advanced Composites Product Data Description HexPly F655 is a bismaleimide resin that cures via an addition reaction in a toughened two-phase thermoset matrix with no condensation
PRODUCT DATASHEET TENCATE E750 PREPREG BENEFITS/FEATURES
PRODUCT TYPE 80 C (176 F) to 180 C (356 F) cure curing toughened epoxy TYPICAL APPLICATIONS Structural applications within Formula 1 SHELF LIFE PRODUCT DESCRIPTION is a toughened epoxy resin system developed
PRODUCT DATA SHEET TYPICAL NEAT RESIN PROPERTIES. Outgassing (TML) % Outgassing (CVCM) % Density g/cc
PRODUCT TYPE 225-250 F (107-121 C) Cure Toughened Cyanate Ester TYPICAL APPLICATIONS High Dimensional Stability Space Structures Optical Benches Reflectors Radomes and Antennae Low Observables Radar Transparent
Advanced General Aviation Transport Experiments
Advanced General Aviation Transport Experiments B Basis Design Allowables for Epoxy Based Prepreg 3M E-Glass Fabric 7781 / SP381 AGATE-WP3.3-033051-098 September 2001 J. Tomblin, J. McKenna, Y. Ng, K.
Effects of Resin and Fabric Structure
Fatigue of Wind Blade Laminates: Effects of Resin and Fabric Structure Details David Miller, Daniel D. Samborsky and John F. Mandell Montana State t University it MCARE 2012 Outline Overview of MSU Fatigue
Advanced General Aviation Transport Experiments
Advanced General Aviation Transport Experiments B-Basis Design Allowables for Wet Layup / Field Repair Fiber Reinforced Composite Material Systems 3K Plain Weave Carbon Cloth / MGS 418 AGATE-WP3.3-033051-115
Failure analysis of serial pinned joints in composite materials
Indian Journal of Engineering & Materials Sciences Vol. 18, April 2011, pp. 102-110 Failure analysis of serial pinned joints in composite materials Alaattin Aktaş* Department of Mechanical Engineering,
MarkForged's Onyx is a material that is ideal for customer-facing parts that need to look good while standing up to industrial requirements.
ONYX MarkForged's Onyx is a material that is ideal for customer-facing parts that need to look good while standing up to industrial requirements. Onyx is based on a remarkably tough nylon, but also provides
CORRELATION BETWEEN RHEOLOGICAL AND MECHANICAL PROPERTIES IN A LOW-TEMPERATURE CURE PREPREG COMPOSITE. A Thesis By. Christopher Ronald Gernaat
CORRELATION BETWEEN RHEOLOGICAL AND MECHANICAL PROPERTIES IN A LOW-TEMPERATURE CURE PREPREG COMPOSITE A Thesis By Christopher Ronald Gernaat Bachelor of Science, Tennessee Technological University 2002
Unified Quiz M4 May 7, 2008 M - PORTION
9:00-10: 00 (last four digits) 32-141 Unified Quiz M4 May 7, 2008 M - PORTION Put the last four digits of your MIT ID # on each page of the exam. Read all questions carefully. Do all work on that question
ASSESSING INTERLAMINAR SHEAR STRESS-STRAIN CURVES IN TAPE COMPOSITES BASED ON THE FLAT-PLATE TORSION METHOD GARY STEVEN GROHMAN JR
ASSESSING INTERLAMINAR SHEAR STRESS-STRAIN CURVES IN TAPE COMPOSITES BASED ON THE FLAT-PLATE TORSION METHOD by GARY STEVEN GROHMAN JR Presented to the Faculty of the Graduate School of The University of
Thermal and mechanical properties of several phthalonitrile resin system
Thermal and mechanical properties of several phthalonitrile resin system Heng Zhou, Feng Liu, Yuehai Li, Tong Zhao* Institute of Chemistry, Chinese Academy of Sciences, Beijing, 100190, China Abstract:An
Non-conventional Glass fiber NCF composites with thermoset and thermoplastic matrices. F Talence, France Le Cheylard, France
20 th International Conference on Composite Materials Copenhagen, 19-24th July 2015 Non-conventional Glass fiber NCF composites with thermoset and thermoplastic matrices. Thierry Lorriot 1, Jalal El Yagoubi
EXPERIMENTALLY DETERMINING THE VISCOELASTIC BEHAVIOR OF A CURING THERMOSET EPOXY R. Thorpe 1, A. Poursartip 1*
19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS EXPERIMENTALLY DETERMINING THE VISCOELASTIC BEHAVIOR OF A CURING THERMOSET EPOXY R. Thorpe 1, A. Poursartip 1* 1 Composites Group, Dept. of Materials
EFFECT OF RETROFITTING ON FLEXURAL RIGIDITY OF RECTANGULAR FRP PLATES
EFFECT OF RETROFITTING ON FLEXURAL RIGIDITY OF RECTANGULAR FRP PLATES STEVEN J. MAKONIS, JR. Department of Civil & Environmental Engineering Old Dominion University Norfolk, VA 23528-0241, USA smako001@odu.edu
Product Selector Guide
Product Selector Guide Encapsulation and casting systems ARALDITE, ARADUR, ARATHERM, ARATHANE www.electrical-insulation-materials.com Encapsulation and casting systems ARALDITE, ARADUR, ARATHERM, ARATHANE
Material Characterization of Natural Fiber Acrylic Thermoset Composites
Material Characterization of Natural Fiber Acrylic Thermoset Composites Andre Bendo Jeremy Funk, John Norton, Dr. Gero Nordmann & Dr. Michael Kalbe BASF Corporation 08/01/2011 1 Presentation verview Key
EMA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 2 Stress & Strain - Axial Loading
MA 3702 Mechanics & Materials Science (Mechanics of Materials) Chapter 2 Stress & Strain - Axial Loading MA 3702 Mechanics & Materials Science Zhe Cheng (2018) 2 Stress & Strain - Axial Loading Statics
[5] Stress and Strain
![[5] Stress and Strain](/thumbs/95/123344550.jpg "[5] Stress and Strain")
[5] Stress and Strain Page 1 of 34 [5] Stress and Strain [5.1] Internal Stress of Solids [5.2] Design of Simple Connections (will not be covered in class) [5.3] Deformation and Strain [5.4] Hooke s Law
IJSER 1. INTRODUCTION. M.Elhadary
1591 A new failure criterion for GRP composite materials subjected to in-phase and out-of-phase biaxial fatigue loading under different stress ratios M.Elhadary Abstract this studying the fatigue behavior
Testing for Equivalence. Purpose of Equivalence CMH17 Statistical Analysis Methods
Testing for Equivalence Purpose of Equivalence CMH17 Statistical Analysis Methods September 14-16, 2010 Safety Awareness Workshop Purpose of Equivalence To demonstrate material equivalency: to assure that
MECE 3321 MECHANICS OF SOLIDS CHAPTER 3
MECE 3321 MECHANICS OF SOLIDS CHAPTER 3 Samantha Ramirez TENSION AND COMPRESSION TESTS Tension and compression tests are used primarily to determine the relationship between σ avg and ε avg in any material.
Synolite 1408-P-1. Product data. DSM Composite Resins
Synolite 8-P- Chemical/physical nature Synolite 8-P- is a low viscous, pre-accelerated, promoted, thixotropic, medium reactive unsaturated polyester resin based on orthophthalic acid. An LSE additive and
D Y N A M I C M E C H A N I C A L A N A L Y S I S A N D I T S A D V A N T A G E S O V E R D E F L E C T I O N T E M P E R A T U R E U N D E R L O A D
D Y N A M I C M E C H A N I C A L A N A L Y S I S A N D I T S A D V A N T A G E S O V E R D E F L E C T I O N T E M P E R A T U R E U N D E R L O A D Sujan E. Bin Wadud TA Instruments 9 Lukens Drive, New
ri [11111 IlL DIRECTIONAL PROPERTIES Of GLASS-FABRIC-BASE PLASTIC LAMINATE PANELS Of SIZES THAT DO NOT IBUCICLE (P-Q1lAtVjr) No.
Supplement to DIRECTIONAL PROPERTIES Of GLASS-FABRIC-BASE PLASTIC LAMINATE PANELS Of SIZES THAT DO NOT IBUCICLE (P-Q1lAtVjr) No. 1803-13 November 1955 This Report is One of a Series issued hi Cooperation
A Report F.I.E.R.O. Total Heat Loss and Evaporative Resistance Measurements of Eight Firefighter Composites. Report #HP
A Report to F.I.E.R.O on Total Heat Loss and Evaporative Resistance Measurements of Eight Firefighter Composites Report #HP170626 from Textile Protection and Comfort Center (T-PACC) College of Textiles
Module III - Macro-mechanics of Lamina. Lecture 23. Macro-Mechanics of Lamina
Module III - Macro-mechanics of Lamina Lecture 23 Macro-Mechanics of Lamina For better understanding of the macromechanics of lamina, the knowledge of the material properties in essential. Therefore, the
MECHANICS OF MATERIALS. Prepared by Engr. John Paul Timola
MECHANICS OF MATERIALS Prepared by Engr. John Paul Timola Mechanics of materials branch of mechanics that studies the internal effects of stress and strain in a solid body. stress is associated with the
Solid Mechanics Homework Answers
Name: Date: Solid Mechanics Homework nswers Please show all of your work, including which equations you are using, and circle your final answer. Be sure to include the units in your answers. 1. The yield
Strength of Material. Shear Strain. Dr. Attaullah Shah
Strength of Material Shear Strain Dr. Attaullah Shah Shear Strain TRIAXIAL DEFORMATION Poisson's Ratio Relationship Between E, G, and ν BIAXIAL DEFORMATION Bulk Modulus of Elasticity or Modulus of Volume
DRAPING SIMULATION. Recent achievements and future trends. Dr. Sylvain Bel LGCIE University Lyon 1
DRAPING SIMULATION Recent achievements and future trends 1 Dr. Sylvain Bel LGCIE University Lyon 1 2 DRAPING SIMULATION Why? How? What? DRAPING SIMULATION WHY? Clamps Punch Fabric Die 1 2 Resin 3 4 Fig.
Effects of Basalt Fibres on Mechanical Properties of Concrete
Effects of Basalt Fibres on Mechanical Properties of Concrete A. M. El-Gelani 1, C.M. High 2, S. H. Rizkalla 3 and E. A. Abdalla 4 1,4 University of Tripoli, Civil Engineering Department, Tripoli, Libya
Effect of Thickness and Fiber Orientation on Flexural Strength of GFRP Composites
Effect of Thickness and Fiber Orientation on Flexural Strength of GFRP Composites Mahesh Chandrashekhar Swamy 1, Parmeshwar Patil 2, Shivaji D. Chame 3, 1 Associate Prof., Dept. of Mechanical Engg., M.S.Bidve
Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on Exam 3.
ES230 STRENGTH OF MTERILS Exam 3 Study Guide Exam 3: Wednesday, March 8 th in-class Updated 3/3/17 Purpose of this Guide: To thoroughly prepare students for the exact types of problems that will be on
If the solution does not follow a logical thought process, it will be assumed in error.
Please indicate your group number (If applicable) Circle Your Instructor s Name and Section: MWF 8:30-9:20 AM Prof. Kai Ming Li MWF 2:30-3:20 PM Prof. Fabio Semperlotti MWF 9:30-10:20 AM Prof. Jim Jones
High Tech High Top Hat Technicians. An Introduction to Solid Mechanics. Is that supposed to bend there?
High Tech High Top Hat Technicians An Introduction to Solid Mechanics Or Is that supposed to bend there? Why don't we fall through the floor? The power of any Spring is in the same proportion with the
Modified Time-temperature Superposition Principle for Viscoelasticity of Thermosetting Resins
The 15 th Composites Durability Workshop (CDW-15), October 17 to 20, 2010, Kanazawa Institute of Technology Modified Time-temperature Superposition Principle for Viscoelasticity of Thermosetting Resins
American Society for Testing and Materials (ASTM) Standards. Mechanical Testing of Composites and their Constituents
Mechanical Testing of Composites and their Constituents American Society for Testing and Materials (ASTM) Standards Tests done to determine intrinsic material properties such as modulus and strength for
CHEM-C2410: Materials Science from Microstructures to Properties Composites: basic principles
CHEM-C2410: Materials Science from Microstructures to Properties Composites: basic principles Mark Hughes 14 th March 2017 Today s learning outcomes To understand the role of reinforcement, matrix and
RESEARCH PROJECT NO. 26
RESEARCH PROJECT NO. 26 DETERMINATION OF POISSON'S RATIO IN AD1 TESTING BY UNIVERSITY OF MICHIGAN REPORT PREPARED BY BELA V. KOVACS and JOHN R. KEOUGH \ MEMBER / / DUCTILE IRON \ SOCIETY Issued by the
THE ROLE OF DELAMINATION IN NOTCHED AND UNNOTCHED TENSILE STRENGTH
THE ROLE OF DELAMINATION IN NOTCHED AND UNNOTCHED TENSILE STRENGTH M. R. Wisnom University of Bristol Advanced Composites Centre for Innovation and Science University Walk, Bristol BS8 1TR, UK M.Wisnom@bristol.ac.uk
TABLE OF CONTENTS. Mechanics of Composite Materials, Second Edition Autar K Kaw University of South Florida, Tampa, USA
Mechanics of Composite Materials, Second Edition Autar K Kaw University of South Florida, Tampa, USA TABLE OF CONTENTS 1. INTRODUCTION TO COMPOSITE MATERIALS 1.1 Introduction... 1.2 Classification... 1.2.1
SOME RESEARCH ON FINITE ELEMENT ANALYSIS OF COMPOSITE MATERIALS
Mechanical Testing and Diagnosis ISSN 2247 9635, 2012 (II), Volume 3, 79-85 SOME RESEARCH ON FINITE ELEMENT ANALYSIS OF COMPOSITE MATERIALS Valeriu DULGHERU, Viorel BOSTAN, Marin GUŢU Technical University
N = Shear stress / Shear strain
UNIT - I 1. What is meant by factor of safety? [A/M-15] It is the ratio between ultimate stress to the working stress. Factor of safety = Ultimate stress Permissible stress 2. Define Resilience. [A/M-15]
EVALUATION OF THE COEFFICIENTS OF MOISTURE EXPANSION USING TRANSIENT SIMULATED LAMINATES METHODOLOGY (TSL)
EVALUATION OF THE COEFFICIENTS OF MOISTURE EXPANSION USING TRANSIENT SIMULATED LAMINATES METHODOLOGY (TSL) Takeshi Takatoya, Kimo Chung, Yi-Jui Wu, and James C. Seferis Polymeric Composites Laboratory,
Analytical Testing Services Commercial Price List ManTech International Corporation January 2018
Analytical ing Services Commercial List ManTech International Corporation January 2018 TABLE OF CONTENTS MECHANICAL TENSILE TESTING... 1 DIFFERENTIAL SCANNING CALORIMETRY (DSC)... 2 THERMOMECHANICAL ANALYSIS
Overview of Probabilistic Modeling of Woven Ceramic Matrix Composites ABSTRACT
ABSTRACT An overview of current research efforts in understanding the cause of variability in the thermo-mechanical properties of woven ceramic matrix composites is presented. Statistical data describing
Chapter. Materials. 1.1 Notations Used in This Chapter
Chapter 1 Materials 1.1 Notations Used in This Chapter A Area of concrete cross-section C s Constant depending on the type of curing C t Creep coefficient (C t = ε sp /ε i ) C u Ultimate creep coefficient
Hilti North America Installation Technical Manual Technical Data MI System Version
MIC-S10-AH-L 179517-1 Hilti North America Installation Technical Manual Technical Data MI System Version 1. 08.017 Terms of common cooperation / Legal disclaimer The product technical data published in
Homework No. 1 MAE/CE 459/559 John A. Gilbert, Ph.D. Fall 2004
Homework No. 1 MAE/CE 459/559 John A. Gilbert, Ph.D. 1. A beam is loaded as shown. The dimensions of the cross section appear in the insert. the figure. Draw a complete free body diagram showing an equivalent
GEOSYNTHETICS ENGINEERING: IN THEORY AND PRACTICE
GEOSYNTHETICS ENGINEERING: IN THEORY AND PRACTICE Prof. J. N. Mandal Department of Civil Engineering, IIT Bombay, Powai, Mumbai 400076, India. Tel.022-25767328 email: cejnm@civil.iitb.ac.in Module-13 LECTURE-
Program: Recent Trends
The SNL/MSU/DOE Fatigue Program: Recent Trends John Mandell Montana State University 2012 SNL Blade Workshop May 30 - June 1, 2012 Outline Overview of MSU Fatigue Program on Wind Blade Materials: Testing
An integrated approach to the design of high performance carbon fibre reinforced risers - from micro to macro - scale
An integrated approach to the design of high performance carbon fibre reinforced risers - from micro to macro - scale Angelos Mintzas 1, Steve Hatton 1, Sarinova Simandjuntak 2, Andrew Little 2, Zhongyi
Comparison of Ply-wise Stress-Strain results for graphite/epoxy laminated plate subjected to in-plane normal loads using CLT and ANSYS ACP PrepPost
Comparison of Ply-wise Stress-Strain results for graphite/epoxy laminated plate subjected to in-plane normal loads using CLT and ANSYS ACP PrepPost 1 Mihir A. Mehta, 2 Satyen D. Ramani 1 PG Student, Department
NUMERICAL DESIGN OF COMPOSITE MATERIALS THROUGH MULTI-SCALE COMPUTER SIMULATION
THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS NUMERICAL DESIGN OF COMPOSITE MATERIALS THROUGH J. Leach 1 *, J. Mackiewicz 2, Dr. S. Risser 1 1 Battelle Memorial Institute, Columbus, OH, USA,
MECHANICS OF MATERIALS
Third E CHAPTER 2 Stress MECHANICS OF MATERIALS Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University and Strain Axial Loading Contents Stress & Strain:
Trace a game-changing discovery
Trace a game-changing discovery Stephen W. Tsai Stanford University October 5, 2015 Topics Why trace? The one and only unifying constant Theory of trace simple; easy to understand C-Ply by Stanford/Chomarat
Part 1 is to be completed without notes, beam tables or a calculator. DO NOT turn Part 2 over until you have completed and turned in Part 1.
NAME CM 3505 Fall 06 Test 2 Part 1 is to be completed without notes, beam tables or a calculator. Part 2 is to be completed after turning in Part 1. DO NOT turn Part 2 over until you have completed and
MECHANICS LAB AM 317 EXP 3 BENDING STRESS IN A BEAM
MECHANICS LAB AM 37 EXP 3 BENDING STRESS IN A BEAM I. OBJECTIVES I. To compare the experimentally determined stresses in a beam with those predicted from the simple beam theory (a.k.a. Euler-Bernoull beam
Failure Analysis of Unidirectional Composite Pinned- Joints
217 IJEDR Volume, Issue 4 ISSN: 2321-9939 Failure Analysis of Unidirectional Composite Pinned- Joints 1 Sai Ashok.M, 2 Mr. U. Koteswara Rao 1 M-tech Machine Design, 2 Associate Professor & Asst. COE 1
HELOXY Epoxy Functional Modifiers
Product Selector HELXY Epoxy Functional Modifiers Momentive's epoxy functional product line of HELXY Modifiers offers formulators the ability to choose between monofunctional and polyfunctional glycidyl
DuPont Zenite LCP. liquid crystal polymer resin PRODUCT AND PROPERTY GUIDE
DuPont Zenite LCP liquid crystal polymer resin PRODUCT AND PROPERTY GUIDE DuPont Zenite LCP liquid crystal polymer resin Description Zenite is the DuPont trademark for its liquid crystal polymer (LCP)
Samantha Ramirez, MSE. Stress. The intensity of the internal force acting on a specific plane (area) passing through a point. F 2
Samantha Ramirez, MSE Stress The intensity of the internal force acting on a specific plane (area) passing through a point. Δ ΔA Δ z Δ 1 2 ΔA Δ x Δ y ΔA is an infinitesimal size area with a uniform force
The Development Of A High Temperature And Acid Resistant Fire Retardant Resin
The Development Of A High Temperature And Acid Resistant Fire Retardant Resin Bruce Curry October 3-6, 2001 ABSTRACT Composites made with polyester and vinyl ester res- ins are resistant to acidic environments.
A fatigue design methodology for GRP composites in offshore underwater applications
A fatigue design methodology for GRP composites in offshore underwater applications Dr P. A. FRIEZE P A F A Consulting Engineers Limited, Hampton, Middx, UK INTRODUCTION Norsk Hydro Troll C field - floating
Donald P. Shiley School of Engineering ME 328 Machine Design, Spring 2019 Assignment 1 Review Questions
Donald P. Shiley School of Engineering ME 328 Machine Design, Spring 2019 Assignment 1 Review Questions Name: This is assignment is in workbook format, meaning you may fill in the blanks (you do not need
Lab Exercise #5: Tension and Bending with Strain Gages
Lab Exercise #5: Tension and Bending with Strain Gages Pre-lab assignment: Yes No Goals: 1. To evaluate tension and bending stress models and Hooke s Law. a. σ = Mc/I and σ = P/A 2. To determine material
Effect of Specimen Dimensions on Flexural Modulus in a 3-Point Bending Test
Effect of Specimen Dimensions on Flexural Modulus in a 3-Point Bending Test M. Praveen Kumar 1 and V. Balakrishna Murthy 2* 1 Mechanical Engineering Department, P.V.P. Siddhartha Institute of Technology,
Prüfmethoden zur Charakterisierung von Verbundwerkstoffen
Prüfmethoden zur Charakterisierung von Verbundwerkstoffen Gerald Pinter 1), Markus Wolfahrt 2) 1) Institut für Werkstoffkunde und Prüfung der Kunststoffe Montanuniversität Leoben, A 2) Polymer Competence
EXPERIMENTAL AND NUMERICAL ANALYSIS OF A LAMINATED BASALT COMPOSITE PLATE SUBJECTED TO BLAST LOAD
2 th International Conference on Composite Materials Copenhagen, 19-24 th July 215 EXPERIMENTAL AND NUMERICAL ANALYSIS OF A LAMINATED BASALT COMPOSITE PLATE SUBJECTED TO BLAST LOAD Süleyman Baştürk 1,
Influence of residual stresses in the structural behavior of. tubular columns and arches. Nuno Rocha Cima Gomes
October 2014 Influence of residual stresses in the structural behavior of Abstract tubular columns and arches Nuno Rocha Cima Gomes Instituto Superior Técnico, Universidade de Lisboa, Portugal Contact:
CARBON FIBER S SURFACE CHEMISTRY AND SELF- ASSEMBLED INTERPHASE FORMATION IN FIBER REINFORCED POLYMER COMPOSITES
THE 19 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS CARBON FIBER S SURFACE CHEMISTRY AND SELF- ASSEMBLED INTERPHASE FORMATION IN FIBER REINFORCED POLYMER COMPOSITES F.N. Nguyen 1*, A.P. Haro 1, D.
Finite Element-Based Failure Models for Carbon/Epoxy Tape Composites
Finite Element-Based Failure Models for Carbon/Epoxy Tape Composites A Master Thesis Presented to The Academic Faculty by Guillaume Seon In Partial Fulfillment of the Requirements for the Degree Master
PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics
![PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics](/thumbs/92/109382806.jpg "PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [ ] Introduction, Fundamentals of Statics")
Page1 PDDC 1 st Semester Civil Engineering Department Assignments of Mechanics of Solids [2910601] Introduction, Fundamentals of Statics 1. Differentiate between Scalar and Vector quantity. Write S.I.
SHEAR CAPACITY OF REINFORCED CONCRETE COLUMNS RETROFITTED WITH VERY FLEXIBLE FIBER REINFORCED POLYMER WITH VERY LOW YOUNG S MODULUS
SHEAR CAPACITY OF REINFORCED CONCRETE COLUMNS RETROFITTED WITH VERY FLEXILE FIER REINFORCED POLYMER WITH VERY LOW YOUNG S MODULUS Hu Shaoqing Supervisor: Susumu KONO ** MEE8165 ASTRACT FRP with low Young
Standard Test Method for Open Hole Tensile Strength of Polymer Matrix Composite Laminates 1
This document is not an ASTM standard and is intended only to provide the user of an ASTM standard an indication of what changes have been made to the previous version. Because it may not be technically
3.2.2 principal material coordinate system, n a coordinate system with axes that are normal to the planes of symmetry inherent to a material
Designation: Standard Test Method for Open Hole Tensile Strength of Polymer Matrix Composite Laminates 1 This standard is issued under the fixed designation D 5766/D 5766M; the number immediately following
Typical Properties T Method
CHO-THERM High Power Thermally Conductive Electrical Insulator Pads Description CHO-THERM HIGH-POWER THERMAL INSULATOR PADS are thermally conductive materials designed for use where the highest possible
Mechanics of Materials
Mechanics of Materials Notation: a = acceleration = area (net = with holes, bearing = in contact, etc...) SD = allowable stress design d = diameter of a hole = calculus symbol for differentiation e = change
FOLDING OF WOVEN COMPOSITE STRUCTURES
FOLDING OF WOVEN COMPOSITE STRUCTURES J.C.H. Yee and S. Pellegrino 1 Department of Engineering, University of Cambridge Trumpington Street, Cambridge CB2 1PZ, UK ABSTRACT This paper investigates one-ply
Modelling of viscoelastic properties of a curing adhesive
Computational Methods and Experiments in Materials Characterisation III 241 Modelling of viscoelastic properties of a curing adhesive J. de Vreugd 1, K. M. B. Jansen 1, L. J. Ernst 1 & J. A. C. M. Pijnenburg
Analysis of Flexural Properties of Carbon Fiber Reinforced / E-Poxy Composite Material
ISSN 2395-1621 Analysis of Flexural Properties of Carbon Fiber Reinforced / E-Poxy Composite Material #1 Kishor Shingare, #2 Dr. S.M. Shendokar, #3 Prof. P.V. Deshmukh, #4 Prof. S.S. Chavan 1 kishorshingare911@gmail.com
COMPRESSION CREEP OF A PULTRUDED E-GLASS/POLYESTER COMPOSITE AT ELEVATED SERVICE TEMPERATURES
COMPRESSION CREEP OF A PULTRUDED E-GLASS/POLYESTER COMPOSITE AT ELEVATED SERVICE TEMPERATURES A Thesis Presented to The Academic Faculty By Kevin Jackson Smith In Partial Fulfillment Of the Requirements
Finite element modelling of infinitely wide Angle-ply FRP. laminates
www.ijaser.com 2012 by the authors Licensee IJASER- Under Creative Commons License 3.0 editorial@ijaser.com Research article ISSN 2277 9442 Finite element modelling of infinitely wide Angle-ply FRP laminates
Steel Cross Sections. Structural Steel Design
Steel Cross Sections Structural Steel Design PROPERTIES OF SECTIONS Perhaps the most important properties of a beam are the depth and shape of its cross section. There are many to choose from, and there
The Accuracy of Characteristic Length Method on Failure Load Prediction of Composite Pinned Joints
, June 30 - July 2, 2010, London, U.K. The Accuracy of Characteristic Length Method on Failure Load Prediction of Composite Pinned Joints O. Aluko, and Q. Mazumder Abstract An analytical model was developed
Section Downloads. Section Downloads. Handouts & Slides can be printed. Other documents cannot be printed Course binders are available for purchase
Level II: Section 04 Simplified Method (optional) Section Downloads Section Downloads Handouts & Slides can be printed Version.0 Other documents cannot be printed Course binders are available for purchase
Thermal loads on optical glass
Version October 2018 1 Introduction In some applications optical glasses have to endure thermal loads: Finishing procedures for optical elements like lenses, prisms, beam splitters and so on involve thermal
NUMERICAL FEM ANALYSIS FOR THE PART OF COMPOSITE HELICOPTER ROTOR BLADE
Journal of KONES Powertrain and Transport, Vol. 19, No. 1 2012 NUMERICAL FEM ANALYSIS FOR THE PART OF COMPOSITE HELICOPTER ROTOR BLADE Hubert D bski Lublin University of Technology, Department of Machine
Passive Damping Characteristics of Carbon Epoxy Composite Plates
Journal of Materials Science and Engineering A 6 (-) 35-4 doi:.765/6-63/6.-.5 D DAVID PUBLISHING Passive Damping Characteristics of Carbon Epoxy Composite Plates Dileep Kumar K * and V V Subba Rao Faculty
Comparison and D 263 T
SCHOTT AG Werk Grünenplan s Comparison and D 263 T D 263 T eco D 263 T remarks Mechanical properties Density ρ in g/cm³ 2.51 2.51 annealed at 40 C/h Stress optical coefficient C in 1.02 10-12 m²/n 3.4
Susterra Propanediol A Renewable Resource for Unsaturated Polyester Resins
TECHNICAL BULLETIN Susterra Propanediol A Renewable Resource for Unsaturated Polyester Resins WILMINGTON, Del., July 9, 2008 Opportunities for Susterra Propanediol (1,3- propanediol) in unsaturated polyester
Mechanical Properties of Materials
Mechanical Properties of Materials Strains Material Model Stresses Learning objectives Understand the qualitative and quantitative description of mechanical properties of materials. Learn the logic of