Analysis of composite materials : application with ANSYS

Gespeichert in:

Autor*in:	Arslan, Mehmet Ali [verfasserIn]

Format:	Buch
Sprache:	Englisch

Erschienen:	New York: MAA ; 2020
Ausgabe:	First edition

Schlagwörter:	Verbundwerkstoff / Mathematisches Modell / Finite-Elemente-Methode / ANSYS

Anmerkung:	Literaturverzeichnis: Seite 423-424
Umfang:	IX, 426 Seiten ; Illustrationen, Diagramme ; 28 cm

Links:	Inhaltsverzeichnis
ISBN:	978-0-9992005-0-6

Katalog-ID:	1728953111

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fulltext	Analysis of Composite Materials Application with ANSYS First Edition Mehmet Ali Arslan, Ph.D. Gebze Technical MAA University Contents Preface … Mechanics of Isotropic Materials Isotropic Materials … ID Uniaxial Stress … 2D Plane Stress … 2D Plane Strain … Mechanics of Orthotropic Materials … ID Uniaxial Stress … 2D Plane Stress … 2D Plane Strain … Analysis of Laminated Composite Structures … Orthotropic Lamina … Stress Transformations … Strain Transformations … Analysis of a General Laminate Using Failure Criteria for Plate … Theory … Composites … Failure Criteria … Maximum Stress Criterion … Maximum Strain Criterion … Tsai-Wu Criterion … Composite … Pressure Vessels/Pipes … Thin-Walled Pressure Vessels … Maximum Stress Criterion … Maximum Stress Criterion … Hygrothermal Analysis … XI … Design I … Design … II of Lamina/Laminate … Hygrothermal Stress-Strain Relation … Mechanical and Hygrothermal Stress-Strain Relation … Analysis of Composite Materials Application - with ANSYS Contents VI … Torsional … Symmetric Beams … Nonsymmetric Sandwich Beams … Composites Symmetric/Nonsymmetric Micromechanics of … Beams … Composites … Particle Reinforced … Fiber Reinforced … Longitudinal Loading … Composites … Composites … Loading Concrete Structures … Reinforced Concretes … Pre-stressed Concretes … Beam Bending Vibrations of Undamped … Natural Beam Modes for … Natural Beam Modes for Different Laminate … Simply Supported Beam … Boundary Conditions … Introduction to ANSYS: Basics … ANSYS Architecture … More … Another Useful … Overview of the ANSYS Commands … Using ANSYS HELP When Needed … More … Composite Beam Bending … Transverse … Composite Laminate Drive Shaft Design … Analysis of Composite Drive Shafts on on … the ANSYS Main Menu Viewing Tool Coordinate Systems … "Pan Zoom Rotate" Beside the ANSYS Bar … Introduction to Geometric … Inputting ANSYS Command Text File When GUI is Open … How … How to Print to Use Cursor Picking Cantilever Beam … or Plot from ANSYS … Solution Steps Using BEAM … Elements (GUI Method) by ANSYS in the Working Directory Solution Steps Solution Using SHELL181 Elements Steps Using SOLID … Elements Appendix- … APDL File … Bending … Files Created … Modeling in ANSYS Navigation Using BEAM … Elements M. Ali Arslan … VII Appendix- … APDL File Using SOLID185 Elements … Using PLANE … APDL File Using PLANE … Elements … APDL File Using SHELL181 Elements … Plane Strain Problem for Solution Steps Using … Elements … Using PLANE … Elements … Using SHELL181 Elements Orthotropic Materials An Orthotropic … Solution - APDL File … Using PLANE … Elements Lamina Under Uniaxial Tensile Steps Using Failure Evaluation of … SHELL281 Elements … Solution Steps Appendix- … Solution Lamina … Using SHELL281 Elements APDL File - Laminate … Using SHELL181 Elements - APDL File … Steps Using SHELL … Elements Appendix- … Hygrothermal Analysis Solution … Using SHELL281 Elements Analysis of Composite APDL File … Analysis Using SHELL281 Elements … Steps Using SHELL181 Elements Appendix- … APDL File Pressure Vessel Failure … Pressure Vessel Failure … Composite Laminate Under Uniaxial Loading Solution Steps Using SHELL281 Elements Appendix- … Loading Appendix- … APDL File Using SHELL281 Elements … Steps Using PLANE … Elements Appendix- … Orthotropic Materials APDL File Plane Strain Problem for Solution … Steps Using SHELL … Elements Appendix- … Isotropic Materials APDL File Plane Stress Problem for Solution … Solution … Isotropic Materials Steps Using SHELL181 Elements … Appendix- … Solution Steps … Using SHELL181 Elements Elements … Appendix- … APDL File Plane Stress Problem for Appendix- … Appendix- … Using SHELL181 Elements … Cross-Ply Laminate Hygrothermal Analysis … Solution Steps Using SHELL281 Elements Appendix- … APDL File Analysis of Using SHELL281 Elements Composite Materials Application - with ANSYS … Contenl VIII … Angle-Ply Laminate Hygrothermal Analysis … Solution Steps Using SHELL … Elements Appendix- … Torsional … Analysis Solution - Torsional … Solution … APDL File Using … SHELL181 Elements … Solution Steps Using SHELL181 Elements … Solution Steps Using SOLSH190 Elements … Appendix- … Appendix- … Sandwich Solution Using SHELL181 Elements … APDL File Using SOLSH … Elements … Solution Problem … Steps Using SOLSH … Elements - Continuous/Aligned A APDL File Composite Analysis APDL File Reinforced … Using SOLSH190 Elements … Composite Analysis … Steps Using SHELL181 Elements - APDL File Composite Strip of Two … Using SHELL181 Elements … Different Materials … Solution Steps Using PLANE … Elements … Solution Steps Using SHELL181 Elements … Appendix- … APDL File Using PLANE … Elements … Appendix- … APDL File Using SHELL181 Elements … The Steel Rod Reinforced Concrete Beam … Analysis … Solution Steps Using BEAM188/REINF264/SOLID185Elements … Solution Steps Using LINK180/SOLID65/SOLID185 Elements … Appendix- … Appendix- … APDL File Using BEAM … REINF264/SOLID185 Elements … APDL File Using LINK180/SOLID65/SOLID185 … Elements Pre-Stressed Concrete Beam … Solution Beam Modal … Steps Using LINK180 and SOLID65 Elements Appendix- … SHELL181 Elements Steps Using SHELL181 Elements Appendix- … Using … APDL File … Analysis of Laminate Appendix- … Bending Analysis of Composite Beam … Steps Using SHELL … Elements Appendix- … Using SHELL181 Elements of Lamina Appendix- … APDL File - APDL File Using LINK … and SOLID65 Elements Analysis with Different Supports (BCs) Solution Steps Using SHELL281 Elements (S-S BCs) M. Ali Arslan … Solution Steps Using SHELL281 Elements (C-F BCs) Appendix- … Appendix- … A - APDL File Using SHELL281 Elements (S-S BCs) … APDL File Using SHELL281 Elements (C-F BCs) … Stepped Cantilever … Solution Beam Deflection … Steps Using SHELL181 Elements … Appendix- … APDL File Using SHELL181 Elements … References … Index … ANSYS Element Types Used in this Book Analysis of … Composite Materials Application - with ANSYS
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code="1">01</subfield><subfield code="x">4370</subfield><subfield code="b">4585929339</subfield><subfield code="c">00</subfield><subfield code="f">--%%--</subfield><subfield code="d">bestellt</subfield><subfield code="e">a</subfield><subfield code="j">--%%--</subfield><subfield code="y">a</subfield><subfield code="z">02-10-24</subfield></datafield><datafield tag="980" ind1=" " ind2=" "><subfield code="2">2001</subfield><subfield code="1">01</subfield><subfield code="x">DE-21</subfield><subfield code="b">4566298515</subfield><subfield code="c">00</subfield><subfield code="f">--%%--</subfield><subfield code="d">64 B 266</subfield><subfield code="e">--%%--</subfield><subfield code="j">--%%--</subfield><subfield code="y">l01</subfield><subfield code="z">15-08-24</subfield></datafield><datafield tag="980" ind1=" " ind2=" "><subfield code="2">2003</subfield><subfield code="1">01</subfield><subfield code="x">DE-25</subfield><subfield code="b">4379017400</subfield><subfield code="c">00</subfield><subfield code="f">--%%--</subfield><subfield code="d">FX 2023/294</subfield><subfield code="e">--%%--</subfield><subfield code="j">--%%--</subfield><subfield code="y">l01</subfield><subfield code="z">26-09-23</subfield></datafield><datafield tag="983" ind1=" " ind2=" "><subfield code="2">21</subfield><subfield code="1">00</subfield><subfield code="x">DE-46</subfield><subfield code="8">30</subfield><subfield code="a">ing 364</subfield></datafield><datafield tag="983" ind1=" " ind2=" "><subfield code="2">100</subfield><subfield code="1">00</subfield><subfield code="x">DE-Ma9</subfield><subfield code="8">00</subfield><subfield code="a">C. 225</subfield></datafield><datafield tag="984" ind1=" " ind2=" "><subfield code="2">21</subfield><subfield code="1">01</subfield><subfield code="x">0046</subfield><subfield code="a">46$0009325719</subfield></datafield><datafield tag="984" ind1=" " ind2=" "><subfield code="2">70</subfield><subfield code="1">01</subfield><subfield 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