The Behavior of Structures Composed of Composite Materials

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The Behavior of
3 _: n4 k' C: Z. \" V6 UStructures Composed of
7 {* d+ e; ]1 o0 m- ^! ^Composite Materials
Second Edition
by
+ q: p. H2 Q5 s3 uJACK R. VINSON
H. Fletcher Brown Porfessor of Mechanical & Aerospace Engineering,
The Center for Composite Materials and The College of Marine Studies,
+ d/ k  A4 t6 nDepartment of Mechanical Engineering,
University of Delaware,
+ l2 L4 j+ a! M* jNewark, Delaware, U.S.A.
4 h. R. X& O# Sand
ROBERT L. SIERAKOWSKI
Chief Scientist,
AFRL/MN Eglin AFB,
) h0 k5 K! V; o7 |: u) ]Florida, U.S.A.
9 |) e' _3 ^2 ^. Z0 W# m

9 p9 p  n: d) m' F
+ z; P* G* |2 Q' ]Contents
% M. g) Q6 }7 {
1. Introduction to Composite Materials 1

3 J( u# B0 d/ Y. N; K, o$ P$ [  DGeneral History
' A' E7 \. F- ~5 vComposite Material Description
Types of Composite Materials
. K% ]* s2 B; S" _! L) aConstituent Properties
- A" Q0 F& D: ^' p  ~' c$ a" b! N6 AComposite Manufacturing, Fabrication and Processing
7 V: p2 m2 @* Y! u9 [9 zUses of Composite Materials
Design and Analyses with Composite Materials
" x7 h, D/ u* D( t) A4 Z. s8 z& i9 eReferences
Journals
Problems
( @2 V% I  d. n; i: |9 o
2. Anisotropic Elasticity and Composite Laminate Theory

Introduction
* N) q, o) O4 K7 J; _, D  X& zDerivation of the Anisotropic Elastic Stiffness and Compliance Matrices
, y  y% O2 Z! h% C0 e% ~2 AThe Physical Meaning of the Components of the Orthotropic Elasticity
) T. b; o; e0 N& u% l% sTensor
" p3 f+ f! @" c( D( zMethods to Obtain Composite Elastic Properties from Fiber and Matrix
Properties
; _' B5 H" U4 ?Thermal and Hygrothermal Considerations
' h+ D- g! S  i9 W! t8 s8 |; iTime-Temperature Effects on Composite Materials
4 m6 L1 _5 `1 g& r% c) ?) Q5 wHigh Strain Rate Effects on Material Properties
' j8 j4 q0 c5 ^9 s, m0 w( [- bLaminae of Composite Materials
1 C) K& ~0 d: M) D# v+ VLaminate Analyses
Piezoelectric Effects
References
Problems
9 t. K8 U. {+ P: e! v
3 P* Y& b' v8 k6 E3. Plates and Panels of Composite Materials
4 z8 S" f7 \9 ~- S
Introduction
; G; j! H' v; `# u! }* cPlate Equilibrium Equations
6 q% n) f" F: X, W; I$ J* y) g) D: GThe Bending of Composite Material Laminated Plates: Classical Theory
Classical Plate Theory Boundary Conditions
Navier Solutions for Rectangular Composite Material Plates
4 L8 ]# N& \# f0 T1 ?1 B5 h' @2 VNavier Solution for a Uniformly Loaded Simply Supported Plate – An
$ K9 D, y9 a- m5 g. ]1 ]Example Problem
( w$ X- b0 d( E5 WLevy Solution for Plates of Composite Materials
9 k5 w8 m* |! r. s  i
Perturbation Solutions for the Bending of a Composite Material Plate With
! D2 L# k1 E4 d( iMid-Plane Symmetry and No Bending-Twisting Coupling
1 t/ }6 D! B8 g0 d% L, YQuasi-Isotropic Composite Panels Subjected to a Uniform Lateral Load
7 f8 A% c7 H2 J5 X/ K. l; |' q  iA Static Analysis of Composite Material Panels Including Transverse
Shear Deformation Effects
3 a. z& t! `/ z  wBoundary Conditions for a Plate Using the Refined Plate Theory Which
) r1 o% d6 _; D$ m7 }9 SIncludes Transverse Shear Deformation
Composite Plates on an Elastic Foundation
6 h& K, h/ j3 i& p- @6 vSolutions 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
/ D& ]4 O' W1 }1 E. J. a5 _Natural Flexural Vibrations of Composite Material Plate Including
Transverse-Shear Deformation Effects
6 _% o" N# M% K1 L- E% p+ IForced-Vibration Response of a Composite Material Plate Subjected to a
9 n8 |) G; G' c  ?+ e8 p# NDynamic Lateral Load
Buckling of a Rectangular Composite Material Plate – Classical Theory
! X6 U2 N  I2 |7 xBuckling of a Composite Material Plate Including Transverse-Shear
Deformation Effects
' ?. y6 p3 a9 N! w4 {Some Remarks on Composite Structures
Methods of Analysis for Sandwich Panels With Composite Material
Faces, and Their Structural Optimization
' h' n, a: K5 F* lGoverning Equations for a Composite Material Plate With Mid-Plane
. Y2 S, N1 u% u7 |) o5 YAsymmetry
Governing Equations for a Composite Material Plate With Bending-
5 {" ~5 X# w6 Q: e' ITwisting Coupling
0 S$ V9 z6 f" c/ S8 B! [- `/ hConcluding Remarks
) y- o: [+ U' H% v& {% TReferences
7 }8 y+ a4 s7 GProblems and Exercises
* x. Z8 g& V7 j6 A- P

% `0 x7 e4 a7 X+ r; @6 E$ E4. Beams, Columns and Rods of Composite Materials

Development of Classical Beam Theory
# v- ~7 G, p) b' L  H2 nSome Composite Beam Solutions
Composite Beams With Abrupt Changes in Geometry or Load
Solutions by Green’s Functions
" `: Y8 e# p0 l( UComposite Beams of Continuously Varying Cross-Section
* o! b* Q- b' W  yRods
( y! g" q  {6 x( K. U( S3 oVibration of Composite Beams
Beams With Mid-Plane Asymmetry
Advanced Beam Theory for Dynamic Loading Including Mid-Plane
0 k; C. Y' q, d& @Asymmetry
, ~2 n$ [% Z4 W+ r9 ~Advanced Beam Theory Including Transverse Shear Deformation Effects
Buckling of Composite Columns
2 ~) d% P8 U5 O8 }, M% mReferences
Problems


! u# F' p7 S# K4 h( f/ \5 T5. Composite Material Shells
% a/ O" d- A5 M& D$ p5 i/ w9 ?* t
7 R1 n: v5 M) V; E0 z4 G+ SIntroduction
Analysis of Composite Material Circular Cylindrical Shells
Some Edge Load and Particular Solutions
/ q& ^' K3 ?7 `6 T% x3 pA General Solution for Composite Cylindrical Shells Under Axially
! X* D: h9 _8 p! V, w3 ^Symmetric Loads
Response of a Long Axi-Symmetric Laminated Composite Shell to an
Edge Displacement
Sample Solutions
, a9 X/ l8 v% [Mid-Plane Asymmetric Circular Cylindrical Shells
Buckling of Circular Cylindrical Shells of Composite Materials Subjected
to Various Loads
Vibrations of Composite Shells
Additional Reading On Composite Shells
References
Problems
6 ^9 r+ i1 t& c3 j/ v) t: S

6. Energy Methods For Composite Material Structures

Introduction
6 z3 K) L2 z' h0 o2 O. J$ F6 sTheorem of Minimum Potential Energy
Analysis of a Beam Using the Theorem of Minimum Potential Energy
; M4 z! X% `8 J9 m9 K, RUse of Minimum Potential Energy for Designing a Composite Electrical
1 p3 k3 x/ {, p8 K6 V( WTransmission Tower
6 Q" B# e7 v+ g5 JMinimum Potential Energy for Rectangular Plates
2 Q5 C: m8 n6 ^4 YA Rectangular Composite Material Plate Subjected to Lateral and
; M; q" l% r* h+ B1 A' }Hygrothermal Loads
# y$ D, V8 R4 n3 d, J% o9 V0 kIn-Plane Shear Strength Determination of Composite Materials in
, w& |, J* L. I% aLaminated Composite Panels
Use of the Theorem of Minimum Potential Energy to Determine Buckling
Loads in Composite Plates
  k3 R' m0 d1 X" }Trial Functions for Various Boundary Conditions for Composite Material
/ m/ F/ X4 }% Y6 W4 k* H0 qRectangular Plates
# j7 d8 ~8 c+ F3 i  yReissner’s Variational Theorem and its Applications
Static Deformation of Moderately Thick Beams
/ L- T7 V5 {' AFlexural Vibrations of Moderately Thick Beams
Flexural Natural Frequencies of a Simply Supported Beam Including
Transverse Shear Deformation and Rotatory Inertia Effects
0 U+ D5 V2 n" iReferences
Problems

. R8 U7 i, ~9 n/ L6 g0 P* S7. Strength and Failure Theories
) D9 d% o4 W! y7 ~' O) f( h
Introduction
* ^: f' b; Z$ z4 iFailure of Monolithic Isotropic Materials
Anisotropic Strength and Failure Theories
Maximum Stress Theory
0 r, n! P( L5 @- k: s, A+ OMaximum Strain Theory
+ w, P2 g& g: m1 A4 e/ AInteractive Failure Theories
: H  X/ Q, V7 P: x/ @6 y( O" BLamina Strength Theories
Laminate Strength Analysis
& V5 g+ f7 a( |8 j7 l) GReferences
Problems
5 @0 A9 W% n9 D# q* l

8. Joining of Composite Material Structures

General Remarks
- w7 r* q5 Z: V) OAdhesive Bonding
Mechanical Fastening
  n2 o' y5 T: z, w4 _* P+ dRecommended Reading
4 H. e% |$ V6 r; SReferences
: E3 V5 r/ ^8 U5 y7 {! wProblems
; }: o7 s# L  ^0 m

: v! S! F) a" W! P  q% i3 v9. Introduction to Composite Design
/ D" L$ B6 ?& t1 Q4 [
( @6 d5 S- Z! v6 J; S5 ]. D$ MIntroduction
! M) `0 t3 N1 X4 H, w5 b- p$ h: E: c, LStructural Composite Design Procedures
, W6 b9 {7 h0 L& I$ gEngineering Analysis
9 b4 e8 K7 \1 PAppendices


) B& }2 B2 m+ \+ S, |+ v3 {& NMicromechanics
Test Standards for Polymer Matrix Composites
5 [" i: \4 E5 S4 i( W& s% {. @- fProperties of Various Polymer Composites
6 g; D% [. e  j& G  X) SAuthor Index
, ]0 w1 G& Z) g8 JSubject Index
3 j, w  l) F( E
[ 本帖最后由 jove20020 于 2008-2-22 23:41 编辑 ]