The Behavior of Structures Composed of Composite Materials

jove20020

The Behavior of
Structures Composed of
0 I. @0 m& h5 N8 @6 D! ^! s( ^Composite Materials
% I; w* W* ~6 u4 z# FSecond Edition
by
JACK R. VINSON
8 F, B7 u) h) v# dH. Fletcher Brown Porfessor of Mechanical & Aerospace Engineering,
The Center for Composite Materials and The College of Marine Studies,
Department of Mechanical Engineering,
University of Delaware,
$ r7 Z& P9 H6 _/ ^6 F9 ANewark, Delaware, U.S.A.
and
5 \9 O# b, S. `: n# j' K# mROBERT L. SIERAKOWSKI
1 ^/ |' G, n( y* Z6 dChief Scientist,
AFRL/MN Eglin AFB,
: v& S% B5 p, G0 ^7 [+ MFlorida, U.S.A.



: Y8 n/ b2 W. P& |6 SContents
6 P6 ]) l2 K1 l0 g! d2 w
1. Introduction to Composite Materials 1
: V; K$ g2 b, C" i
7 R' y5 W  T& m$ bGeneral History
Composite Material Description
8 c6 y4 w! ^- O0 J" n/ ]2 l6 qTypes of Composite Materials
Constituent Properties
- v) R. }+ w5 J& b' t& z- ?Composite Manufacturing, Fabrication and Processing
Uses of Composite Materials
Design and Analyses with Composite Materials
References
Journals
/ `. t" T) B, m; [6 i& {8 g. m2 ?Problems

6 X* a6 A8 |* ^1 O- R& Q5 f9 I$ z2. Anisotropic Elasticity and Composite Laminate Theory
: F' L2 g9 s& [& W4 j# z
: v1 h8 t# W# |) D/ b: YIntroduction
Derivation of the Anisotropic Elastic Stiffness and Compliance Matrices
9 D2 f1 L7 N4 F( P/ ^' XThe Physical Meaning of the Components of the Orthotropic Elasticity
* _5 e0 U% p# m2 E. S5 n- rTensor
$ p* ~$ [9 y2 w3 ]$ l' m0 nMethods to Obtain Composite Elastic Properties from Fiber and Matrix
Properties
4 e% j, c' ], N2 ]Thermal and Hygrothermal Considerations
Time-Temperature Effects on Composite Materials
High Strain Rate Effects on Material Properties
$ {' l! k2 m% D& x, sLaminae of Composite Materials
Laminate Analyses
Piezoelectric Effects
# i: S9 \1 s% o) Y+ e  j6 DReferences
2 S) G" h0 A) w, g6 V" [- rProblems

2 J3 W0 w; F, H8 d- y3. Plates and Panels of Composite Materials

Introduction
; s! u' n" G: iPlate Equilibrium Equations
0 T- b7 D0 m9 f+ |3 k8 E- xThe Bending of Composite Material Laminated Plates: Classical Theory
Classical Plate Theory Boundary Conditions
Navier Solutions for Rectangular Composite Material Plates
Navier Solution for a Uniformly Loaded Simply Supported Plate – An
! U+ i. e' {' C9 j: v/ \Example Problem
Levy Solution for Plates of Composite Materials

+ U; C. Z: |  D: HPerturbation Solutions for the Bending of a Composite Material Plate With
Mid-Plane Symmetry and No Bending-Twisting Coupling
# q' B4 g/ g5 I! d# gQuasi-Isotropic Composite Panels Subjected to a Uniform Lateral Load
A Static Analysis of Composite Material Panels Including Transverse
Shear Deformation Effects
5 m% C- \# R8 VBoundary Conditions for a Plate Using the Refined Plate Theory Which
$ S2 F; ^4 w7 c4 w8 U8 S& fIncludes Transverse Shear Deformation
Composite Plates on an Elastic Foundation
Solutions for Plates of Composite Materials Including Transverse-Shear
# `+ x' `7 `) _. s4 S5 CDeformation Effects, Simply Supported on All Four Edges
' g3 D6 |' G' ?4 o* r$ ]. a# l; iDynamic Effects on Panels of Composite Materials
, k/ ^: b0 h, I$ A4 h) W; p' oNatural Flexural Vibrations of Rectangular Plates: Classical Theory
Natural Flexural Vibrations of Composite Material Plate Including
Transverse-Shear Deformation Effects
' u5 x6 w( r' @: R" G) cForced-Vibration Response of a Composite Material Plate Subjected to a
Dynamic Lateral Load
# }$ j* p% s2 n( v) I# Q) dBuckling of a Rectangular Composite Material Plate – Classical Theory
! ]; W8 [' G/ e8 n+ KBuckling of a Composite Material Plate Including Transverse-Shear
Deformation Effects
9 h% l1 S3 B. X: W! E6 n8 [Some Remarks on Composite Structures
Methods of Analysis for Sandwich Panels With Composite Material
Faces, and Their Structural Optimization
Governing Equations for a Composite Material Plate With Mid-Plane
; X" s2 e/ r7 V6 YAsymmetry
7 |2 }2 }; Z: t& Z. ?8 HGoverning Equations for a Composite Material Plate With Bending-
Twisting Coupling
Concluding Remarks
References
Problems and Exercises
8 h+ o0 A! o' j% n

& I$ C+ c6 ^: @6 u( L+ t2 {: M4. Beams, Columns and Rods of Composite Materials
9 P+ o- s, S$ t% d  s8 r
  N' j7 S3 X# [& `& F" z% YDevelopment of Classical Beam Theory
Some Composite Beam Solutions
# B$ c. \% O/ C' s8 `- w' sComposite Beams With Abrupt Changes in Geometry or Load
Solutions by Green’s Functions
" {- x# L9 }; EComposite Beams of Continuously Varying Cross-Section
Rods
Vibration of Composite Beams
, m; Z3 m+ L) d6 g& o3 p: B! kBeams With Mid-Plane Asymmetry
3 A0 L1 A; t. U5 b5 \: HAdvanced Beam Theory for Dynamic Loading Including Mid-Plane
Asymmetry
Advanced Beam Theory Including Transverse Shear Deformation Effects
Buckling of Composite Columns
  U# j& n/ o: [2 H3 @( f) {References
: Q/ ?5 M2 V) \5 s" q& q8 P3 QProblems

3 C8 W$ x' H& {1 M" M+ @- U
5. Composite Material Shells
7 h' o% L- k* g7 L/ H
: o. @; R, ]7 r9 B4 y) X: f' SIntroduction
3 F3 Z' n% }  g  U% u$ HAnalysis of Composite Material Circular Cylindrical Shells
+ G; A2 t: e0 o) lSome Edge Load and Particular Solutions
* n  B  M2 ~/ TA General Solution for Composite Cylindrical Shells Under Axially
3 S* @5 y& h; k9 n6 [3 r# wSymmetric Loads
: m. J6 c7 ?9 N! k  z0 jResponse of a Long Axi-Symmetric Laminated Composite Shell to an
# @8 o& S6 a+ u/ ?% m! o2 nEdge Displacement
4 }3 z$ w! P  i8 }Sample Solutions
Mid-Plane Asymmetric Circular Cylindrical Shells
Buckling of Circular Cylindrical Shells of Composite Materials Subjected
to Various Loads
" N* {/ s. T7 Z( fVibrations of Composite Shells
Additional Reading On Composite Shells
References
Problems
- c( A) V: E  W/ s1 P

6. Energy Methods For Composite Material Structures

  ~% d" A2 ]3 L; I0 x: }( t+ VIntroduction
% ^8 N4 [* E- v; b- H/ B6 `Theorem of Minimum Potential Energy
Analysis of a Beam Using the Theorem of Minimum Potential Energy
6 t4 `9 @0 X2 `- rUse of Minimum Potential Energy for Designing a Composite Electrical
Transmission Tower
Minimum Potential Energy for Rectangular Plates
7 ?8 f4 U3 c6 E2 N/ J- \2 jA Rectangular Composite Material Plate Subjected to Lateral and
' u0 T8 i7 B2 rHygrothermal Loads
In-Plane Shear Strength Determination of Composite Materials in
4 P& I2 d% B' H2 R6 U8 F3 ?, @Laminated Composite Panels
Use of the Theorem of Minimum Potential Energy to Determine Buckling
Loads in Composite Plates
9 P7 B; \4 O1 \$ D6 p, e, h0 JTrial Functions for Various Boundary Conditions for Composite Material
Rectangular Plates
Reissner’s Variational Theorem and its Applications
8 y* N7 T# u4 I% E: O. DStatic Deformation of Moderately Thick Beams
1 L" ]& i' Y/ _3 J$ ]( x$ V0 kFlexural Vibrations of Moderately Thick Beams
Flexural Natural Frequencies of a Simply Supported Beam Including
& I# |: r7 x$ r# O9 k2 l) {+ u2 uTransverse Shear Deformation and Rotatory Inertia Effects
5 p  V' z' G3 C/ rReferences
Problems

7. Strength and Failure Theories

0 c7 f& S5 B' d; p& r: LIntroduction
9 c6 ?* v; V' S' p% MFailure of Monolithic Isotropic Materials
Anisotropic Strength and Failure Theories
Maximum Stress Theory
Maximum Strain Theory
+ C/ r- g7 O7 x  K3 O2 A+ ~Interactive Failure Theories
Lamina Strength Theories
Laminate Strength Analysis
References
) @$ p& e9 c. I) UProblems
0 F: @# u1 z$ J9 }  M2 w, v6 e

4 P4 y. k/ L" Y8. Joining of Composite Material Structures
9 @4 f7 p! T6 m" U  w: A
General Remarks
1 O$ p: K) s6 GAdhesive Bonding
6 D  `0 n5 g6 ?, u* `: r/ ~1 O2 m6 GMechanical Fastening
Recommended Reading
( c* ^/ o; v  M, G/ eReferences
Problems


$ g! `$ Z  @- ^6 Z8 m9. Introduction to Composite Design

Introduction
5 x+ a  _( K0 E2 S$ X7 }Structural Composite Design Procedures
# {- C- X- W! k) iEngineering Analysis
Appendices
5 p) b+ l- h0 n0 v( O5 r8 P
  ?' E1 L% t' y; X  e. c
9 D; P$ Y6 {, e2 ^: G: xMicromechanics
Test Standards for Polymer Matrix Composites
Properties of Various Polymer Composites
Author Index
% ~; W, c  t3 C* Z, y3 {( GSubject Index
, v( o% O* y+ l- Z( p
[ 本帖最后由 jove20020 于 2008-2-22 23:41 编辑 ]