The Behavior of Structures Composed of Composite Materials

jove20020

The Behavior of
Structures Composed of
- {1 o9 }/ d! z* M' x6 w4 R7 NComposite Materials
; m& h* |+ s: a0 }  o; M; KSecond Edition
by
JACK R. VINSON
H. Fletcher Brown Porfessor of Mechanical & Aerospace Engineering,
The Center for Composite Materials and The College of Marine Studies,
Department of Mechanical Engineering,
6 ^% i; ?. ~& c! a- i5 p" h7 C- SUniversity of Delaware,
& o+ _& ]) [% u& r2 S) N) u. |Newark, Delaware, U.S.A.
and
ROBERT L. SIERAKOWSKI
2 R4 t* p2 ?* h! qChief Scientist,
AFRL/MN Eglin AFB,
Florida, U.S.A.



2 Q9 W1 J) ?% H  A8 \* rContents

1. Introduction to Composite Materials 1
# g3 h6 j7 }( P& H  H
) K2 T3 x  J0 E) H6 t, E$ {General History
# Q  A6 P3 o; `# nComposite Material Description
2 Y. a8 Q+ ~, ~( w/ GTypes of Composite Materials
) E' G, k( A6 C. O4 t# V7 p0 Y; [Constituent Properties
) p1 b3 E4 o* {# H5 mComposite Manufacturing, Fabrication and Processing
Uses of Composite Materials
Design and Analyses with Composite Materials
References
Journals
0 u- M( e9 k( x9 W" Q% rProblems

3 ^3 Z$ W! j- A# f1 r2. Anisotropic Elasticity and Composite Laminate Theory

Introduction
" M/ n# T7 L, C) n# kDerivation of the Anisotropic Elastic Stiffness and Compliance Matrices
4 ]9 j2 E; V7 |6 w/ d8 _; |+ H# U7 PThe Physical Meaning of the Components of the Orthotropic Elasticity
, B8 A0 \% C/ o% @Tensor
Methods to Obtain Composite Elastic Properties from Fiber and Matrix
* ~5 x2 {, F0 |Properties
! B/ _2 J( C/ ^# H6 gThermal and Hygrothermal Considerations
Time-Temperature Effects on Composite Materials
4 z5 [6 _5 C# b" A- B7 y6 oHigh Strain Rate Effects on Material Properties
2 }! g9 B. ~' J+ pLaminae of Composite Materials
Laminate Analyses
Piezoelectric Effects
# H' C4 q7 K" O% U1 `3 _7 lReferences
, v& ~( E" `- ~. D% EProblems

3. Plates and Panels of Composite Materials

7 K* x6 Y4 W' l! i" z) v0 R( v  K- AIntroduction
Plate Equilibrium Equations
* R7 J, \  L! [' m  Q" d- G8 LThe Bending of Composite Material Laminated Plates: Classical Theory
Classical Plate Theory Boundary Conditions
Navier Solutions for Rectangular Composite Material Plates
, s. @- }. @' f. wNavier Solution for a Uniformly Loaded Simply Supported Plate – An
' U9 n/ ?( ^# B% n9 h7 a) vExample Problem
6 k, z( E' X7 A" mLevy Solution for Plates of Composite Materials

Perturbation Solutions for the Bending of a Composite Material Plate With
) F- T3 K3 a. h+ s0 w* ^& V. w( \Mid-Plane Symmetry and No Bending-Twisting Coupling
; y, S* A2 _: Q$ f1 f3 fQuasi-Isotropic Composite Panels Subjected to a Uniform Lateral Load
% [1 r* ^0 q3 O# w2 K5 kA Static Analysis of Composite Material Panels Including Transverse
# b# ~# }+ ]* ?9 g3 ?- `' b; AShear Deformation Effects
Boundary Conditions for a Plate Using the Refined Plate Theory Which
- W4 ^2 r2 R% _7 `* Q! jIncludes Transverse Shear Deformation
) j0 W$ S. A1 ~! C2 HComposite Plates on an Elastic Foundation
1 E6 Y9 J4 Q4 sSolutions for Plates of Composite Materials Including Transverse-Shear
* X7 N7 E! X( ]% J3 j9 i- r4 HDeformation Effects, Simply Supported on All Four Edges
/ k5 ]" {5 u: E, k, r2 V  p' dDynamic Effects on Panels of Composite Materials
Natural Flexural Vibrations of Rectangular Plates: Classical Theory
/ s2 u2 k& r7 I9 y1 b# N& BNatural Flexural Vibrations of Composite Material Plate Including
9 i4 F5 E  j: x2 O$ R; D3 Z. PTransverse-Shear Deformation Effects
' \( m0 i9 F6 |9 Y1 n; ?Forced-Vibration Response of a Composite Material Plate Subjected to a
Dynamic Lateral Load
$ [6 Q5 q, r" c% f6 o$ QBuckling of a Rectangular Composite Material Plate – Classical Theory
3 Q8 ?  j4 {% F& SBuckling of a Composite Material Plate Including Transverse-Shear
9 ]$ ~% {; ]2 NDeformation Effects
Some Remarks on Composite Structures
) g( A- Y0 J. D+ c  {' Q* M$ \Methods of Analysis for Sandwich Panels With Composite Material
Faces, and Their Structural Optimization
Governing Equations for a Composite Material Plate With Mid-Plane
Asymmetry
3 C6 ~& j5 a" |' v$ uGoverning Equations for a Composite Material Plate With Bending-
) ~* D: u# |1 T+ x, y6 \2 KTwisting Coupling
( P. ~! M& v0 d/ ~% LConcluding Remarks
References
Problems and Exercises
" S% f, P) y+ ]9 w. s( X; _

% I9 D% O0 p; G8 T) C* e$ R, ?, x8 x4. Beams, Columns and Rods of Composite Materials
) k4 H* H' v8 k, m7 Y. r/ u9 ^
Development of Classical Beam Theory
- ^: _/ V: P/ N+ qSome Composite Beam Solutions
4 O3 W7 }; |0 a1 J) M6 F! QComposite Beams With Abrupt Changes in Geometry or Load
% w$ ~& a0 x- e7 @$ ?- lSolutions by Green’s Functions
' \/ q# N$ C+ ]" w/ O) ?( jComposite Beams of Continuously Varying Cross-Section
' G" x/ `8 \/ N- e( d( D. p: p4 XRods
* P1 M/ L( `. UVibration of Composite Beams
" x7 `5 n/ ]9 a( [Beams With Mid-Plane Asymmetry
Advanced Beam Theory for Dynamic Loading Including Mid-Plane
6 K/ J% M# s. y, T0 ^" U% DAsymmetry
Advanced Beam Theory Including Transverse Shear Deformation Effects
9 {' x* c; g9 S, n; \2 {Buckling of Composite Columns
) {0 k( I- u8 G: pReferences
$ O' B8 {& h" S3 j+ {9 DProblems

, U6 b  Y% g" Q9 `, i* v4 J
$ ^) J- j% E* q8 m8 i) p. g5. Composite Material Shells

( c8 P/ L+ j. W! _Introduction
Analysis of Composite Material Circular Cylindrical Shells
Some Edge Load and Particular Solutions
A General Solution for Composite Cylindrical Shells Under Axially
# v% r# c/ v) n) aSymmetric Loads
Response of a Long Axi-Symmetric Laminated Composite Shell to an
Edge Displacement
: u4 U. R" u9 g8 s% n$ o' Z4 f, X/ DSample Solutions
Mid-Plane Asymmetric Circular Cylindrical Shells
% V0 m) g0 \  P. d5 L. R" N/ TBuckling of Circular Cylindrical Shells of Composite Materials Subjected
to Various Loads
8 v8 [* |& w, ?' v% ?Vibrations of Composite Shells
, D4 L! H3 i4 _# U- ?% V! [Additional Reading On Composite Shells
6 j5 ]7 e/ H6 tReferences
/ P; w- M4 s" `! F$ J, gProblems


5 s; ^8 w- U: R6. Energy Methods For Composite Material Structures
! O+ |1 l: k* G6 x+ y' N
Introduction
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
Transmission Tower
8 M9 c) q+ U" }3 U  W1 P. NMinimum Potential Energy for Rectangular Plates
A Rectangular Composite Material Plate Subjected to Lateral and
Hygrothermal Loads
; R) M" Q, ^4 X! F5 v  R: rIn-Plane Shear Strength Determination of Composite Materials in
Laminated Composite Panels
Use of the Theorem of Minimum Potential Energy to Determine Buckling
* c6 G7 [. E  A- Y, u; a  cLoads in Composite Plates
- ~4 y3 ~1 X1 H5 DTrial Functions for Various Boundary Conditions for Composite Material
4 R( a! _4 |; o2 D; fRectangular Plates
Reissner’s Variational Theorem and its Applications
Static Deformation of Moderately Thick Beams
* ]1 V8 i- i% U6 p9 u1 f2 e. P# kFlexural Vibrations of Moderately Thick Beams
  {  h6 n/ V: B( P& t( T% B1 iFlexural Natural Frequencies of a Simply Supported Beam Including
Transverse Shear Deformation and Rotatory Inertia Effects
" ~3 W  X9 Y& E. l: oReferences
Problems
: W8 O! L" b, {/ i9 N
7 d0 D0 e4 z- U9 G7. Strength and Failure Theories
. f9 Y! _# _/ A  ~6 {$ C( {
8 y, x& r+ @" e0 yIntroduction
Failure of Monolithic Isotropic Materials
( _" p3 I5 W" c2 X  `6 X5 S" [Anisotropic Strength and Failure Theories
Maximum Stress Theory
Maximum Strain Theory
8 t/ d. ]) j7 a( g8 u) L9 gInteractive Failure Theories
# z: D& I* z* f1 M5 XLamina Strength Theories
! B  A2 B, r0 Z0 |$ {8 H- `Laminate Strength Analysis
References
# q. c" E+ H2 B/ ZProblems


& n8 N9 n5 c; b+ p4 N8. Joining of Composite Material Structures
# r- n& H# n3 G$ N
2 w2 X5 Y: G4 o! b( x' ?6 yGeneral Remarks
Adhesive Bonding
0 S# e* l2 ?# x/ K2 mMechanical Fastening
Recommended Reading
7 j2 z( l" u& t! `! ?0 T! B) }References
Problems
6 S" @/ [/ N, g* ~4 B  |

3 k& O+ H4 |. G5 R0 j9. Introduction to Composite Design
6 s$ a; y" x$ K! A
Introduction
/ m5 ]# y' F0 [4 z& Z" W  vStructural Composite Design Procedures
Engineering Analysis
Appendices


0 w# L5 f& t  _; V" H( C" }Micromechanics
3 y* n# V- i; q* YTest Standards for Polymer Matrix Composites
Properties of Various Polymer Composites
Author Index
Subject Index

[ 本帖最后由 jove20020 于 2008-2-22 23:41 编辑 ]