The Behavior of Structures Composed of Composite Materials

jove20020

The Behavior of
6 W0 Q! x8 S' H0 w7 c. [; WStructures Composed of
Composite Materials
& v! N" X/ @# [, i. V' t. ~$ qSecond Edition
$ u( D$ L; r; Q3 n1 Sby
JACK R. VINSON
! f" D( }; `: KH. Fletcher Brown Porfessor of Mechanical & Aerospace Engineering,
The Center for Composite Materials and The College of Marine Studies,
Department of Mechanical Engineering,
6 Z# c+ q; H0 ?" I$ A; O' TUniversity of Delaware,
Newark, Delaware, U.S.A.
and
ROBERT L. SIERAKOWSKI
7 L1 @6 |) k# i) v6 MChief Scientist,
AFRL/MN Eglin AFB,
Florida, U.S.A.



% D; E3 o6 T, j% i+ B5 f3 ?: jContents

- `3 B4 E# s/ x5 j0 G2 y, z6 w1. Introduction to Composite Materials 1

General History
/ W& k3 p1 K: M  _1 i, NComposite Material Description
9 Q9 n5 C0 u6 A8 ]% iTypes of Composite Materials
Constituent Properties
Composite Manufacturing, Fabrication and Processing
Uses of Composite Materials
. s! H# A+ o# a  d3 uDesign and Analyses with Composite Materials
* x5 Z3 w" Y+ y* E3 u& XReferences
- t0 C+ E  m& v# ?/ G' HJournals
Problems

7 }! k1 |# J" Q% ]* c  z* z2. Anisotropic Elasticity and Composite Laminate Theory

Introduction
5 M; h1 a8 `% B* Q6 ]7 HDerivation of the Anisotropic Elastic Stiffness and Compliance Matrices
8 f' l' o' m# Z: BThe Physical Meaning of the Components of the Orthotropic Elasticity
! Q4 z' B% _3 i7 k# X8 qTensor
Methods to Obtain Composite Elastic Properties from Fiber and Matrix
' L) m; ^* S* A6 p) `( I' l) MProperties
2 y* |. x% Y9 L) J$ a* ZThermal and Hygrothermal Considerations
3 ~* B2 Z8 W! V$ u+ I7 a0 JTime-Temperature Effects on Composite Materials
High Strain Rate Effects on Material Properties
Laminae of Composite Materials
Laminate Analyses
! b8 F& ^  X/ l$ S2 H" TPiezoelectric Effects
References
Problems

+ y( Y" q6 X* o- _; V4 @) J3. Plates and Panels of Composite Materials

Introduction
Plate Equilibrium Equations
/ B+ D; `; v3 |% MThe Bending of Composite Material Laminated Plates: Classical Theory
Classical Plate Theory Boundary Conditions
1 ^+ o0 p6 T1 I. X0 e2 V8 I% t! k, JNavier Solutions for Rectangular Composite Material Plates
Navier Solution for a Uniformly Loaded Simply Supported Plate – An
( p& ^! D. E, @! ]  F; |( i7 q: rExample Problem
Levy Solution for Plates of Composite Materials

/ H. p8 H7 b5 N9 r$ w4 D6 b+ oPerturbation Solutions for the Bending of a Composite Material Plate With
; Y# g0 A" x6 n$ P/ w( d/ _& uMid-Plane Symmetry and No Bending-Twisting Coupling
$ T. F. n2 I/ K  {2 H7 z5 }Quasi-Isotropic Composite Panels Subjected to a Uniform Lateral Load
A Static Analysis of Composite Material Panels Including Transverse
Shear Deformation Effects
: `+ l3 d- t: ~) i) {% Q  HBoundary Conditions for a Plate Using the Refined Plate Theory Which
: N3 m& y4 X. J: J2 |; kIncludes Transverse Shear Deformation
Composite Plates on an Elastic Foundation
8 v! g  }0 C0 t! d' l7 C# b! tSolutions for Plates of Composite Materials Including Transverse-Shear
Deformation Effects, Simply Supported on All Four Edges
Dynamic Effects on Panels of Composite Materials
Natural Flexural Vibrations of Rectangular Plates: Classical Theory
Natural Flexural Vibrations of Composite Material Plate Including
Transverse-Shear Deformation Effects
$ G5 T8 J4 X0 [+ J8 r/ bForced-Vibration Response of a Composite Material Plate Subjected to a
, I- V7 ~6 e  \' U& ]* LDynamic Lateral Load
Buckling of a Rectangular Composite Material Plate – Classical Theory
9 D$ K5 o/ {/ q0 w; A8 E/ kBuckling of a Composite Material Plate Including Transverse-Shear
# O/ H4 n; A7 Y  p4 f3 ~Deformation Effects
: ?1 n: P3 k: k( p1 E/ s& j" mSome 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
8 n  D' e% Y2 N: a' f: JAsymmetry
Governing Equations for a Composite Material Plate With Bending-
Twisting Coupling
Concluding Remarks
# Y0 b7 _( i* {/ {References
Problems and Exercises


4. Beams, Columns and Rods of Composite Materials

Development of Classical Beam Theory
" v9 _6 k) d! a8 }1 XSome Composite Beam Solutions
Composite Beams With Abrupt Changes in Geometry or Load
Solutions by Green’s Functions
0 I  q  T3 ~) n8 DComposite Beams of Continuously Varying Cross-Section
Rods
/ S3 ~9 R& k/ }; T* x' xVibration of Composite Beams
% I/ N5 P7 b/ X: c# p9 e& p, QBeams With Mid-Plane Asymmetry
Advanced Beam Theory for Dynamic Loading Including Mid-Plane
* _( _* N4 t6 W0 i& F, D( w+ x: p0 CAsymmetry
Advanced Beam Theory Including Transverse Shear Deformation Effects
8 g) ], R  u6 a" M) T6 K* k# rBuckling of Composite Columns
/ M& J# X6 k* K  y, JReferences
Problems

* s% ^' K3 z5 M6 N
5. Composite Material Shells
, ]  [& t  }  \' ?
& }* z5 J& E. N0 o; d1 zIntroduction
6 f4 ~5 v* e+ E5 zAnalysis of Composite Material Circular Cylindrical Shells
Some Edge Load and Particular Solutions
A General Solution for Composite Cylindrical Shells Under Axially
) `- C& f8 C+ z  N- D) E+ X2 H, o  a+ ZSymmetric Loads
Response of a Long Axi-Symmetric Laminated Composite Shell to an
Edge Displacement
Sample Solutions
# ^( z9 N; g: }% OMid-Plane Asymmetric Circular Cylindrical Shells
Buckling of Circular Cylindrical Shells of Composite Materials Subjected
to Various Loads
6 f% T4 y* r& ^9 y. A5 rVibrations of Composite Shells
1 J! z6 D9 f$ J- N# P) y1 EAdditional Reading On Composite Shells
) O. F9 |' Y3 n/ ~4 @7 J2 n; qReferences
" y; ]" e" Y$ i0 d4 \Problems

0 ~. a9 U# Y' ?$ l* r) ?
0 ?9 o0 Z! c2 R/ Z8 j8 `6. Energy Methods For Composite Material Structures
* r! ~3 F6 J1 @7 U" N( c' o% K
Introduction
Theorem of Minimum Potential Energy
Analysis of a Beam Using the Theorem of Minimum Potential Energy
( [8 v5 F# V! }0 |Use of Minimum Potential Energy for Designing a Composite Electrical
Transmission Tower
+ @/ g: }* H9 JMinimum Potential Energy for Rectangular Plates
A Rectangular Composite Material Plate Subjected to Lateral and
Hygrothermal Loads
# Z/ m& |9 N  C( IIn-Plane Shear Strength Determination of Composite Materials in
Laminated Composite Panels
' ?/ w$ |8 N! d: j2 @" l; AUse of the Theorem of Minimum Potential Energy to Determine Buckling
Loads in Composite Plates
Trial Functions for Various Boundary Conditions for Composite Material
Rectangular Plates
- {* f. B+ R" P( `8 R. t, ]4 vReissner’s Variational Theorem and its Applications
Static Deformation of Moderately Thick Beams
; d- U' }1 H; W& }& dFlexural Vibrations of Moderately Thick Beams
Flexural Natural Frequencies of a Simply Supported Beam Including
% |% a! R' [' p  O$ tTransverse Shear Deformation and Rotatory Inertia Effects
References
9 f" _* O1 F/ B3 T: iProblems
% [5 m9 N; ?1 v: q. i) d# h
0 N7 g5 Y' L, C3 g; u1 _2 e$ M0 L7. Strength and Failure Theories
* V9 N& S, T) O  D# W
! ^/ N  N, h8 L( oIntroduction
! V8 I; t& }  \) q& n. l6 KFailure of Monolithic Isotropic Materials
3 Z4 q/ R0 N% @# Z1 j* CAnisotropic Strength and Failure Theories
Maximum Stress Theory
% e% F2 L7 \. L3 m% Z9 k' PMaximum Strain Theory
2 n5 Z% Y  L1 `/ nInteractive Failure Theories
: e* N8 n1 m! j8 A: |+ {8 S  gLamina Strength Theories
Laminate Strength Analysis
( W5 s! S2 ~* l0 g2 FReferences
* @) f8 v* O# F  B, G" U7 gProblems

; W8 v; n4 d8 w# {; t& H
' [  k5 O- ?" _: n8. Joining of Composite Material Structures

2 E1 L' L" A7 U% y( f' y- VGeneral Remarks
: D8 R0 Q5 w# ]Adhesive Bonding
Mechanical Fastening
Recommended Reading
References
) Q3 [, o& F1 j0 o6 q5 |+ i8 ?Problems


; z: X- O! |, e8 g% o& p8 \7 k9. Introduction to Composite Design

! k9 W( M- G# ?) TIntroduction
Structural Composite Design Procedures
Engineering Analysis
' J& P6 o/ `2 K+ y. ~9 QAppendices

! s* `- o1 }, O  a! Q1 [
Micromechanics
Test Standards for Polymer Matrix Composites
* G0 m7 b+ L+ n) D; U+ k) P8 aProperties of Various Polymer Composites
Author Index
9 N  E' c9 ?3 d' t( |& {Subject Index

  \" p' @7 Y" f2 ?8 i" U. [8 N[ 本帖最后由 jove20020 于 2008-2-22 23:41 编辑 ]