The Behavior of Structures Composed of Composite Materials

jove20020

The Behavior of
7 {) U/ X0 _4 Q: Q! TStructures Composed of
Composite Materials
+ S" r' Y8 h: o; P' VSecond Edition
by
. B' C# n4 _5 v8 |JACK R. VINSON
" b. r& X0 K/ BH. Fletcher Brown Porfessor of Mechanical & Aerospace Engineering,
The Center for Composite Materials and The College of Marine Studies,
Department of Mechanical Engineering,
6 k" v6 Q7 O0 v0 a$ H$ o3 j8 A! dUniversity of Delaware,
1 |/ n: }/ v  H! R( _  tNewark, Delaware, U.S.A.
  T/ }! `, }1 d/ d- F: D4 m2 W9 Band
0 F+ S4 O9 o8 ]% X1 P0 QROBERT L. SIERAKOWSKI
Chief Scientist,
( F# v% G( @7 N! w0 F: v6 ], a' oAFRL/MN Eglin AFB,
& X- S8 c% |2 A- ]4 AFlorida, U.S.A.
/ \1 d& u; `; U
) H0 a$ k3 ^, C+ d& P

Contents
3 r1 I, a' D. E" j* q  V" Y
2 @8 X- l8 G. l7 r0 t1. Introduction to Composite Materials 1
1 H4 z  x1 }5 g1 M' B. E- w, X
; Z* ~: O1 S$ u; i1 Y, ^4 SGeneral History
! ~" o9 v, p7 W; M* O8 wComposite Material Description
Types of Composite Materials
Constituent Properties
Composite Manufacturing, Fabrication and Processing
Uses of Composite Materials
+ B  s$ g) y! ~( b. @. Q3 h' }Design and Analyses with Composite Materials
References
! P/ K8 o' u) l+ }) `Journals
Problems

2. Anisotropic Elasticity and Composite Laminate Theory
, }& @8 Z. _, z3 j
3 O) V# R$ ?2 e4 b2 rIntroduction
+ X# }9 l, J& j& A# C! E" q) hDerivation of the Anisotropic Elastic Stiffness and Compliance Matrices
The Physical Meaning of the Components of the Orthotropic Elasticity
# N, U5 v$ U, {7 gTensor
Methods to Obtain Composite Elastic Properties from Fiber and Matrix
Properties
Thermal and Hygrothermal Considerations
Time-Temperature Effects on Composite Materials
High Strain Rate Effects on Material Properties
$ `% i& H1 I$ \) A) ULaminae of Composite Materials
" o  g8 t: S# |$ P+ q9 N, MLaminate Analyses
, n9 `' W* E0 j3 [2 I& ?Piezoelectric Effects
+ Y$ ^( d! i; w' g$ l: ?References
) C' M! c8 R- _( x5 D. e6 G/ QProblems
3 {$ {) {1 k8 ?4 Y8 o
3. Plates and Panels of Composite Materials

9 f) i2 n8 N1 a, a. bIntroduction
  ]5 F' D! [; _- ^, @; g2 Q4 q" ]Plate Equilibrium Equations
- ?% ?0 I% d* G: d8 O: AThe Bending of Composite Material Laminated Plates: Classical Theory
" s7 D; w4 F/ D% v5 v- n# MClassical Plate Theory Boundary Conditions
( q8 k0 Z+ g+ `" I! {Navier Solutions for Rectangular Composite Material Plates
, {  ]- `& |+ J( `) jNavier Solution for a Uniformly Loaded Simply Supported Plate – An
Example Problem
Levy Solution for Plates of Composite Materials

Perturbation Solutions for the Bending of a Composite Material Plate With
( C5 L* V: G* J: T$ O/ U' wMid-Plane Symmetry and No Bending-Twisting Coupling
Quasi-Isotropic Composite Panels Subjected to a Uniform Lateral Load
A Static Analysis of Composite Material Panels Including Transverse
3 }; `0 q6 u0 o/ g4 W; _$ EShear Deformation Effects
Boundary Conditions for a Plate Using the Refined Plate Theory Which
Includes Transverse Shear Deformation
Composite Plates on an Elastic Foundation
" ^5 D& r% n" D9 y1 r& c) BSolutions for Plates of Composite Materials Including Transverse-Shear
Deformation Effects, Simply Supported on All Four Edges
2 F; y- u) e1 w5 U; |, dDynamic Effects on Panels of Composite Materials
& [& c# x5 _# W9 UNatural Flexural Vibrations of Rectangular Plates: Classical Theory
5 \  i% W' c5 A, [8 z! G: g9 WNatural Flexural Vibrations of Composite Material Plate Including
Transverse-Shear Deformation Effects
Forced-Vibration Response of a Composite Material Plate Subjected to a
! q( |  U4 V# P9 ], [Dynamic Lateral Load
Buckling of a Rectangular Composite Material Plate – Classical Theory
# P; [* i, V; |2 UBuckling of a Composite Material Plate Including Transverse-Shear
& i! V7 |! b+ SDeformation Effects
* p* _$ I( V+ f( ~: K1 SSome Remarks on Composite Structures
! y2 s/ V; c" l9 _7 AMethods of Analysis for Sandwich Panels With Composite Material
( m# G+ D2 y: c* O$ p1 [' C7 V5 d' MFaces, and Their Structural Optimization
! x6 D: y( s% j3 E2 ~Governing Equations for a Composite Material Plate With Mid-Plane
' p& G5 x' p0 x3 |3 _$ r) vAsymmetry
1 `" @8 x9 D* ?# O7 cGoverning Equations for a Composite Material Plate With Bending-
! t% F' H% V$ }: c1 hTwisting Coupling
Concluding Remarks
# Q0 O4 E8 K# C/ nReferences
Problems and Exercises
; z# X" m+ p9 x1 m7 h- R6 X
. B# [! ^, x6 K0 z' S
0 i) u& x0 T( u5 `6 X! v* `3 Z4. Beams, Columns and Rods of Composite Materials
5 Q2 G8 Q  t; H& N8 n
Development of Classical Beam Theory
( y; g4 z/ B  @) W6 s" G7 mSome Composite Beam Solutions
, G$ G/ h! O' {' R6 \Composite Beams With Abrupt Changes in Geometry or Load
+ V8 o- s' [2 Z7 ~Solutions by Green’s Functions
( D3 I! N1 R5 m# e# X+ iComposite Beams of Continuously Varying Cross-Section
8 u- _- N1 d3 A8 i- G! O2 \Rods
Vibration of Composite Beams
Beams With Mid-Plane Asymmetry
% J# c  [' ^( {& G& b; V' n# _- [+ QAdvanced Beam Theory for Dynamic Loading Including Mid-Plane
Asymmetry
( {3 Z7 h4 n) r0 N6 NAdvanced Beam Theory Including Transverse Shear Deformation Effects
Buckling of Composite Columns
7 t" v' @/ t5 v) E" x* t0 UReferences
: N6 E% D/ N# M: z- ?, YProblems


5. Composite Material Shells

( E3 R  }- L( Q# u' @& @Introduction
Analysis of Composite Material Circular Cylindrical Shells
Some Edge Load and Particular Solutions
A General Solution for Composite Cylindrical Shells Under Axially
2 v$ a: K: R+ H7 z- D) rSymmetric Loads
. n: ?4 _1 z5 {8 O# X8 WResponse of a Long Axi-Symmetric Laminated Composite Shell to an
7 V6 Z. Z9 t; _- n3 m5 ?Edge Displacement
Sample Solutions
Mid-Plane Asymmetric Circular Cylindrical Shells
Buckling of Circular Cylindrical Shells of Composite Materials Subjected
to Various Loads
Vibrations of Composite Shells
7 H, s. g& u' ]7 B; AAdditional Reading On Composite Shells
9 c' i1 O3 o9 D) S- NReferences
, d7 H: l& m4 e5 {. J# pProblems


6. Energy Methods For Composite Material Structures
/ ], L* x; S. f  @. A6 y
- I# @- r8 H3 q0 K7 X, sIntroduction
Theorem of Minimum Potential Energy
Analysis of a Beam Using the Theorem of Minimum Potential Energy
Use of Minimum Potential Energy for Designing a Composite Electrical
6 ^' C$ v# M; m6 vTransmission Tower
# S) r- N6 m+ y% J- [  GMinimum Potential Energy for Rectangular Plates
& B! p6 |% |) S" D/ l/ K. y5 fA Rectangular Composite Material Plate Subjected to Lateral and
5 I) Z( |6 Z* ]+ YHygrothermal Loads
- B2 [5 L, w# P, X5 M( z4 zIn-Plane Shear Strength Determination of Composite Materials in
Laminated Composite Panels
Use of the Theorem of Minimum Potential Energy to Determine Buckling
Loads in Composite Plates
: K' O; u: |2 C  f2 X- STrial Functions for Various Boundary Conditions for Composite Material
Rectangular Plates
Reissner’s Variational Theorem and its Applications
Static Deformation of Moderately Thick Beams
Flexural Vibrations of Moderately Thick Beams
$ Y  |! y3 k1 E7 [8 u0 CFlexural Natural Frequencies of a Simply Supported Beam Including
Transverse Shear Deformation and Rotatory Inertia Effects
* Y* R% Q" ?) t6 Y: AReferences
, r5 |. E6 g3 ?6 G) a+ S' G0 SProblems

7. Strength and Failure Theories
. X5 c! r1 r5 Y2 F
* x* h& s6 {9 F; h. J; n) mIntroduction
Failure of Monolithic Isotropic Materials
Anisotropic Strength and Failure Theories
Maximum Stress Theory
9 c6 [; U  ?8 B+ I) x! WMaximum Strain Theory
Interactive Failure Theories
Lamina Strength Theories
Laminate Strength Analysis
, Z1 g4 s5 w4 N+ a' d+ D. nReferences
& k% ^; j- s1 _+ a3 fProblems
' z2 P* R% g& W2 T) ]& k! O

8. Joining of Composite Material Structures

General Remarks
! G; I" U6 p- Z# rAdhesive Bonding
Mechanical Fastening
  Y5 b" h6 _& {+ P* z) kRecommended Reading
! I) Z4 G  G: g! t' JReferences
; D" k# W4 {: v. eProblems
' J+ V& |& b$ R" `: P$ D

7 B5 f, R! k0 M9. Introduction to Composite Design

9 t$ X+ @) m3 D1 l1 iIntroduction
Structural Composite Design Procedures
# m6 @' t: G4 \! b9 A/ A" f2 rEngineering Analysis
Appendices
( h7 l- ]  p4 P- ~! {

9 \+ R! }- j7 j2 u& jMicromechanics
) a& P0 `% Z4 [( r, `& b: H9 ITest Standards for Polymer Matrix Composites
Properties of Various Polymer Composites
/ v/ S( T# I) F( l) v3 xAuthor Index
- C1 ]2 F+ F+ Q) QSubject Index
, D' d& P3 S* q8 o# P' }
[ 本帖最后由 jove20020 于 2008-2-22 23:41 编辑 ]