The Behavior of Structures Composed of Composite Materials

jove20020

The Behavior of
Structures Composed of
Composite Materials
Second Edition
$ K, |/ H1 ~- i/ S6 ]3 j9 B+ l/ D" Rby
* Z1 x& u8 q0 X  [. t3 f7 M) [# ?JACK R. VINSON
H. Fletcher Brown Porfessor of Mechanical & Aerospace Engineering,
2 x; K) y6 [$ oThe Center for Composite Materials and The College of Marine Studies,
Department of Mechanical Engineering,
University of Delaware,
Newark, Delaware, U.S.A.
  o, V, G, x- `6 Kand
9 ~7 `0 \( Y% u7 iROBERT L. SIERAKOWSKI
Chief Scientist,
5 z2 i3 K5 D+ }/ H8 l* JAFRL/MN Eglin AFB,
Florida, U.S.A.
2 i1 h6 X$ J. b& J) B8 I6 W& r3 B3 o
8 {" ~5 g9 L/ I9 h$ P5 q4 c$ x& Q

+ B7 S6 e# V& e7 h/ Z6 dContents
2 A  T( q. B7 \: H2 S% R
1. Introduction to Composite Materials 1

General History
% u+ U* m2 ^# k3 X4 `Composite Material Description
Types of Composite Materials
, `% y. Q/ O/ A2 E* B3 cConstituent Properties
Composite Manufacturing, Fabrication and Processing
& P4 b- W9 h" ], bUses of Composite Materials
9 x/ H% y: k: p0 B* \Design and Analyses with Composite Materials
References
9 @- Y: j' W" R; T9 k6 I9 a2 B. SJournals
$ {& H6 |4 s) c% c0 y# o" GProblems
. _7 V& g$ j* D: k
5 n+ s! g+ D8 n) X! I) }% s; G. \2. Anisotropic Elasticity and Composite Laminate Theory
8 {2 _* G+ t3 k
  o0 W6 |3 t8 z; H& HIntroduction
Derivation of the Anisotropic Elastic Stiffness and Compliance Matrices
The Physical Meaning of the Components of the Orthotropic Elasticity
" ~, ]1 C0 z* zTensor
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
Laminae of Composite Materials
Laminate Analyses
* u6 v( r, _9 ?, ^0 LPiezoelectric Effects
* o6 _/ ^! Y- h4 N+ U; QReferences
/ `7 z2 B; s. @3 ^Problems
7 p3 y) M1 ?$ y0 A
3. Plates and Panels of Composite Materials

Introduction
5 V8 v  I0 M' tPlate Equilibrium Equations
, e5 P) L, x2 ]3 X( ]% s! dThe Bending of Composite Material Laminated Plates: Classical Theory
5 B1 v0 i+ ]5 ]1 w+ G( c" [+ s7 N6 cClassical Plate Theory Boundary Conditions
Navier Solutions for Rectangular Composite Material Plates
& ~; P+ o) S: E) lNavier Solution for a Uniformly Loaded Simply Supported Plate – An
Example Problem
Levy Solution for Plates of Composite Materials

# R' B; B" U2 n6 Y/ l' H% }Perturbation Solutions for the Bending of a Composite Material Plate With
Mid-Plane Symmetry and No Bending-Twisting Coupling
Quasi-Isotropic Composite Panels Subjected to a Uniform Lateral Load
( p* q( ]% ^; E8 x* l; iA Static Analysis of Composite Material Panels Including Transverse
) z5 ]  M* A6 K- p/ {2 fShear Deformation Effects
Boundary Conditions for a Plate Using the Refined Plate Theory Which
Includes Transverse Shear Deformation
Composite Plates on an Elastic Foundation
! y# h7 L. R9 u* L3 e' zSolutions for Plates of Composite Materials Including Transverse-Shear
Deformation Effects, Simply Supported on All Four Edges
Dynamic Effects on Panels of Composite Materials
' E5 M: }3 x. s1 f1 y) j+ Z( gNatural Flexural Vibrations of Rectangular Plates: Classical Theory
) ?. y2 \2 g' H/ G' hNatural Flexural Vibrations of Composite Material Plate Including
; f3 y- e& L  P" T9 {/ YTransverse-Shear Deformation Effects
Forced-Vibration Response of a Composite Material Plate Subjected to a
1 e) D4 s. x* A; h! |' N# cDynamic Lateral Load
0 b1 A) l. F- x1 C/ S) }Buckling of a Rectangular Composite Material Plate – Classical Theory
Buckling of a Composite Material Plate Including Transverse-Shear
Deformation Effects
5 Z5 b0 q2 C. \* \1 w' YSome Remarks on Composite Structures
4 R9 |  S2 @' }, M' n$ J8 [' HMethods of Analysis for Sandwich Panels With Composite Material
) S8 D8 g; a" V+ S2 YFaces, and Their Structural Optimization
% \, B  W& E- [, y- FGoverning Equations for a Composite Material Plate With Mid-Plane
2 D6 G' I! k- H* d( tAsymmetry
7 v. J2 k; ~; J4 B, q4 e6 ]Governing Equations for a Composite Material Plate With Bending-
# B; q/ M2 g/ ~2 ?# ~Twisting Coupling
Concluding Remarks
* m5 o8 j2 L( C- P9 j1 J% S% MReferences
7 H! U" I2 s  |Problems and Exercises
3 l) E( o4 _# g, w

! [) D3 V) v% Z" S4. Beams, Columns and Rods of Composite Materials
% Y( P9 }: q- S& v3 x+ N+ R! D
Development of Classical Beam Theory
Some Composite Beam Solutions
Composite Beams With Abrupt Changes in Geometry or Load
Solutions by Green’s Functions
8 P/ K( F# g& |9 _* C3 tComposite Beams of Continuously Varying Cross-Section
$ a" D! p; X% TRods
Vibration of Composite Beams
Beams With Mid-Plane Asymmetry
8 {1 l9 j( H9 W9 m2 s* @0 xAdvanced Beam Theory for Dynamic Loading Including Mid-Plane
Asymmetry
Advanced Beam Theory Including Transverse Shear Deformation Effects
; ?* }5 T8 g7 pBuckling of Composite Columns
- ~* h" Z% B$ }/ o4 IReferences
Problems


8 _. |- \% n" M- _2 s3 {) |5. Composite Material Shells
# e8 E( W) r* n4 S* b$ t# W; T
2 h, G+ Z# Y1 j" w2 GIntroduction
8 g" `1 B& t" ?' [0 IAnalysis of Composite Material Circular Cylindrical Shells
Some Edge Load and Particular Solutions
+ m0 Q( U% p7 k4 ZA General Solution for Composite Cylindrical Shells Under Axially
Symmetric Loads
8 n) B6 r. S; jResponse of a Long Axi-Symmetric Laminated Composite Shell to an
Edge Displacement
- n3 g" W4 J/ `* T6 i! _- q8 JSample Solutions
Mid-Plane Asymmetric Circular Cylindrical Shells
Buckling of Circular Cylindrical Shells of Composite Materials Subjected
to Various Loads
# ]$ e* M5 {) z* b+ |1 {Vibrations of Composite Shells
Additional Reading On Composite Shells
: f6 q5 R& R7 n8 ]3 r3 JReferences
Problems

) i& c, v5 C$ e1 o/ l
6. Energy Methods For Composite Material Structures

Introduction
Theorem of Minimum Potential Energy
# ]. V2 E( x; n9 H5 EAnalysis of a Beam Using the Theorem of Minimum Potential Energy
% L' f: @; ]6 j" E( L. q* s# ~Use of Minimum Potential Energy for Designing a Composite Electrical
6 ?3 a& g. `  R! X: u4 s' S% t- DTransmission Tower
  F2 s" B# ~( M! I9 v0 {* T% L7 e' _Minimum Potential Energy for Rectangular Plates
4 N. C: R& A7 ]7 U& ~. {+ @A Rectangular Composite Material Plate Subjected to Lateral and
! k0 L) H# z1 _Hygrothermal Loads
2 w6 m9 W  r0 T4 {2 I- V. s( eIn-Plane Shear Strength Determination of Composite Materials in
! k! Q3 d" `! v# ?  FLaminated Composite Panels
Use 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
Reissner’s Variational Theorem and its Applications
Static Deformation of Moderately Thick Beams
Flexural Vibrations of Moderately Thick Beams
Flexural Natural Frequencies of a Simply Supported Beam Including
+ I9 N$ M9 K( G1 LTransverse Shear Deformation and Rotatory Inertia Effects
4 Q& B4 J# ^! z, c/ pReferences
Problems
4 b1 C% f) C3 T
7. Strength and Failure Theories

0 Q: P) v, N: k- LIntroduction
Failure of Monolithic Isotropic Materials
Anisotropic Strength and Failure Theories
Maximum Stress Theory
Maximum Strain Theory
Interactive Failure Theories
* W! Z# W4 ^5 K' D$ k$ GLamina Strength Theories
9 x! H! K; O3 ALaminate Strength Analysis
- x+ a9 @1 ]7 [. {! y6 wReferences
8 ?+ {; w4 F$ [  jProblems

' X- O0 a, _7 ^1 S. s- G' {6 J
8. Joining of Composite Material Structures

1 |: p  W. d5 J9 F4 oGeneral Remarks
Adhesive Bonding
Mechanical Fastening
Recommended Reading
) @' a: s1 @1 p& @References
+ Z# Z( S. V1 k- qProblems
- {3 e6 q3 W! C1 }0 h
7 L* ^; }; O$ k
# B% S1 A! N$ ?9. Introduction to Composite Design
" x4 J& b6 L  v( f) T
Introduction
# ~, H) B8 m# F  Z! k6 W3 u( xStructural Composite Design Procedures
Engineering Analysis
2 S4 ?+ q; C2 v2 \+ D* PAppendices
; o  U# g% N) i6 \; H
' n- \3 q) |: X
* N" R' ~0 {3 D  K% @. fMicromechanics
% D$ m/ h, t1 LTest Standards for Polymer Matrix Composites
Properties of Various Polymer Composites
% f, K6 D) F5 dAuthor Index
Subject Index
9 B5 B0 f& V6 v4 D
1 ]4 r  C# ~. X; S' A[ 本帖最后由 jove20020 于 2008-2-22 23:41 编辑 ]