![Delamination; Modelling;
Finite element; Beams;
Piezoelectrics
1.0 INTRODUCTION
1.1. General information
The development of active structural
health monitoring systems and
techniques using piezoelectric actuator
and sensor wafers or films is an area
experiencing significant technical
activity[1 a]. Particular emphasis is
placed on the active structural health
monitoring methods for composite
structures, as the likelihood of internal
defects, and the evolution of invisible
damage in the composite material
during service life remains high. One
candidate type of damage is
delamination cracks, which are
usually induced during low-velocity
impact and fatigue, remain hidden and
can propagate quickly leading to
catastrophic failure. Among the many
open issues in this field is the
development of analytical and
numerical models capable of capturing
the effect of delaminations on the
structural response, particularly on
the electromechanical response
components associated with the
piezoelectric actuators and sensors, as
such models may help understand the
sensitivity of electromechanical
response on damage parameters, and
thus provide a basis for the
development of damage detection and
localization techniques and the design of
the smart composite system. To this
end, this paper presents a layerwise
mechanics theory and a finite element
for analyzing laminated beams with
delamination cracks and active
piezoelectric sensors.
In the present paper, an
electromechanically coupled
layerwise theory is described for
composite beams with piezoelectric
actuators and sensors, treating
interfacial sliding, crack opening and
slope discontinuity across a
delamination crack, as additional
degrees of freedom. The generalized
stiffness, mass piezoelectric, and
permittivity matrices are formulated and
a 2-node finite element is further
developed. The new finite element
capabilities are evaluated by predicting
the effect of a single delamination on
the modal and quasistatic response of
composite beams with passive or
active piezoelectric layers. The](https://image.slidesharecdn.com/moodlegeneralisedformulationoflaminatetheoryusingbeamfefordelaminatedcompositebeamswithpie-120517071420-phpapp01/85/Moodle-generalised-formulation-of-laminate-theory-using-beam-fe-for-delaminated-composite-beams-with-pie-2-320.jpg)
![3.1.Materials, geometry, and
assumptions:
This section presents numerical results
from several representative problems.
The accuracy of the developed
mechanics is first validated for the case
of pristine beams with previous models.
Predicted modal frequencies of
delaminated beams are also compared
with previously contacted experimental
results [1 b]. All applications were
focused on composite Gr/Epoxy
T300/934 beams with quasi-isotropic
laminations [0/90/45/_45]s, 0.127 mm
nominal ply thickness, 280 mm long and
25 mm wide. Four different full-width
delamination crack sizes were used (see
Fig. 2) covering the 10.9%, 21.8%
and 43.6% of the total specimen‟s
length, respectively. In the composite
beams two piezoceramic layers were
considered each one covering the top
and bottom surface of the specimen
having thickness equal to the nominal
ply thickness. The piezoceramic layers
were used either as actuators or sensors.
4.0 ILLUSTRATION](https://image.slidesharecdn.com/moodlegeneralisedformulationoflaminatetheoryusingbeamfefordelaminatedcompositebeamswithpie-120517071420-phpapp01/85/Moodle-generalised-formulation-of-laminate-theory-using-beam-fe-for-delaminated-composite-beams-with-pie-5-320.jpg)
Moodle generalised formulation of laminate theory using beam fe for delaminated composite beams with pie
- 1. GENERALISED FORMULATION OF LAMINATE THEORY USING BEAM FE FOR DELAMINATED COMPOSITE BEAMS WITH PIEZO ACTUATORS AND PIEZO SENSORS B. Kavi, B. K. Nanda Research Scholar Department of Mechanical Engineering NIT, Rourkela 769008 Professor Department of Mechanical Engineering NIT, Rourkela 769008 E-mail: binit.kavi@gmail.com E-mail: bknanda@nitrkl.ac.in ABSTRACT A coupled linear layer wise laminate theory and a beam FE are formulated for analyzing delaminated composite beams with piezoactuators and sensors. The model assumes zigzag fields for the axial displacements and the electric potential and it treats the discontinuities in the displacement fields due to the delaminations as additional degrees of freedom. The formulation naturally includes the excitation of piezoelectric actuators, their interactions with the composite laminate, and the effect of delamination on the predicted sensory voltage. The quasistatic and modal response of laminated composite Gr/Epoxy beams with active or sensory layers having various delamination sizes is predicted. The numerical results illustrate the strong effect of delamination on the sensor voltage, on through the thickness displacement and on the stress fields. Finally, the effect of delamination on modal frequencies and shapes are predicted and compared with previously obtained experimental results. Keywords: Composite materials; Laminate;
- 2. Delamination; Modelling; Finite element; Beams; Piezoelectrics 1.0 INTRODUCTION 1.1. General information The development of active structural health monitoring systems and techniques using piezoelectric actuator and sensor wafers or films is an area experiencing significant technical activity[1 a]. Particular emphasis is placed on the active structural health monitoring methods for composite structures, as the likelihood of internal defects, and the evolution of invisible damage in the composite material during service life remains high. One candidate type of damage is delamination cracks, which are usually induced during low-velocity impact and fatigue, remain hidden and can propagate quickly leading to catastrophic failure. Among the many open issues in this field is the development of analytical and numerical models capable of capturing the effect of delaminations on the structural response, particularly on the electromechanical response components associated with the piezoelectric actuators and sensors, as such models may help understand the sensitivity of electromechanical response on damage parameters, and thus provide a basis for the development of damage detection and localization techniques and the design of the smart composite system. To this end, this paper presents a layerwise mechanics theory and a finite element for analyzing laminated beams with delamination cracks and active piezoelectric sensors. In the present paper, an electromechanically coupled layerwise theory is described for composite beams with piezoelectric actuators and sensors, treating interfacial sliding, crack opening and slope discontinuity across a delamination crack, as additional degrees of freedom. The generalized stiffness, mass piezoelectric, and permittivity matrices are formulated and a 2-node finite element is further developed. The new finite element capabilities are evaluated by predicting the effect of a single delamination on the modal and quasistatic response of composite beams with passive or active piezoelectric layers. The
- 3. analytical predictions of the modal frequencies are further correlated with available measurements. Also the delamination mode shapes are presented showing the delamination „„breathing‟‟. Through these model predictions, some mechanisms capable of revealing the delamination presence are further discussed with an eye toward active delamination detection. 2.0 EQUATIONS AND SYMBOLS This section presents the formulated mechanics for piezoelectric laminated beams with interlaminar delamination cracks. 2.1. Governing material equations Each ply is assumed to exhibit linear piezoelectric behavior. In the current beam case, in-plane and interlaminar shear strains are considered in the elastic field. The piezoelectric materials considered are monoclinic class two crystals with the poling direction coincident with the z-axis. The constitutive equations have the form 1, 5 and S1, S5 are the axial and shear mechanical stresses and strains, respectively; E1 and E3 are the electric field vectors; D1 and D3 are the electric displacement vectors; C11 and C55 are the elastic stiffness coefficients; e15 and e31 are the piezoelectric coefficients; and 11, 33 are the electric permittivity coefficients of the material. Superscripts E and S indicate constant electric field and strain conditions, respectively. The above system of equations encompasses the behavior of a beam‟s piezocomposite layer. The electric field vector is the negative gradient of the electric potential 2.2. Equations of equilibrium
- 4. 2.3. Kinematic assumptions 2.4. Strain–displacement relations and electrical field 2.5. Laminate electric enthalpy and laminate matrices 2.6. Finite element formulation 3.0 APPLICATIONS AND DISCUSSION In the present paper, we focus on the quasistatic response ( =0)and free dynamic response (P(t) = Q(t) = θ A(t) = 0) of the delaminated beam.
- 5. 3.1.Materials, geometry, and assumptions: This section presents numerical results from several representative problems. The accuracy of the developed mechanics is first validated for the case of pristine beams with previous models. Predicted modal frequencies of delaminated beams are also compared with previously contacted experimental results [1 b]. All applications were focused on composite Gr/Epoxy T300/934 beams with quasi-isotropic laminations [0/90/45/_45]s, 0.127 mm nominal ply thickness, 280 mm long and 25 mm wide. Four different full-width delamination crack sizes were used (see Fig. 2) covering the 10.9%, 21.8% and 43.6% of the total specimen‟s length, respectively. In the composite beams two piezoceramic layers were considered each one covering the top and bottom surface of the specimen having thickness equal to the nominal ply thickness. The piezoceramic layers were used either as actuators or sensors. 4.0 ILLUSTRATION
- 7. 4.0 SUMMARY
- 8. Layerwise mechanics were formulated and described for analyzing the coupled electromechanical response of delaminated composite beams with embedded passive or active piezoelectric layers. Delamination crack movements (relative slip and opening) were included in the mechanics as additional degrees of freedom. The capability and versatility of the new finite element to model the effect of delamination on the modal and quasistatic response was evaluated on Gr/Epoxy T300 composite beams with various sizes of delamination cracks. Modal frequency predictions were favorably correlated with previously contacted experimental measurements. Numerical studies of the effect of delamination on local fields evaluated the capabilities of the method and pointed out some promising damage indicators. Usage of a network of piezoceramic or piezopolymer sensors covering the surface of a critical structural area appears promising in the low-frequency region, provided that proper modes are excited and monitored. Voltage variations across the length of the beam may offer information about the axial position and the boundaries of delamination, which can be exemplified by proper actuator configurations. On the other hand, axial and shear strain or stress distribution appear far more sensitive to the vertical and horizontal position of debonding. Combination of the information offered from the sensory voltage and the axial or shear strains may effectively reveal the position and size of a delamination. An additional damage index may be the sensor voltage distribution of a beam actuated near a breathing modal frequency. Overall, the developed FE offers many advantages toward the simulation and design of active delamination monitoring structures. Future work has been directed toward the inclusion of interfacial contact into the mechanics and FE, and the prediction of the non-linear dynamic response. 5.0 REFERENCES 1. a. Nikolaos, Chrysochoidis, Dimitris, Saravanos, “Generalized layerwise mechanics for the static and modal response of delaminated composite beams with active piezoelectric sensors”, International Journal of Solids and Structures 44, 2007, pp. 8751–8768.
- 9. b. Chrysochoidis, Saravanos, “Assessing the effects of delamination on the damped dynamic response of composite beams with piezoelectric actuators and sensors”, Smart materials and Structures 13 (4), 2004, pp. 733–742. 2. a. Jinquan Cheng, Farid Taheri, “A smart single-lap adhesive joint integrated with partially distributed piezoelectric patches”, International Journal of Solids and Structures 43, 2006, pp. 1079–1092. b. Jinquan Cheng, Xiaoxia Wu , Guoqiang Li, Farid Taheri, Su-Seng Pang, ” Development of a smart composite pipe joint integrated with piezoelectric layers under tensile loading”, International Journal of Solids and Structures 43, 2006, pp 5370–5385. 3. G. Song, V. Sethi, H.-N. Li,“Vibration control of civil structures using piezoceramic smart materials: A review”, Engineering Structures 28, 2006, pp. 1513–1524.