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Nondestructive Evaluation and Health Monitoring of Advanced
Structures (NDE & SHM) |
Every engineered
structure, no matter how well constructed, contains hidden
flaws that are caused by its manufacturing process, service
loads and degradation of its material due to aging. The
safety and integrity of a structure can be severely
compromised by the growth of these flaws unless they are
detected and the structure is repaired at an early stage of
their initiation. As an example, foreign object impact or
fatigue loading in advanced composite structures can
introduce hidden delaminations that can grow to a critical
size and result in a catastrophic failure of the structure.
Another area of concern is the rapidly increasing inventory
of aging structures in both military and civilian
applications, and there is increasing demand for extending
their service life. Life extension of aging aircraft,
aerospace and civil structures require an early detection of
defects in their critical components through inspection and
maintenance at regular intervals that are very costly and
often ineffective or unnecessary. The life cycle cost of new
and aging structures can greatly reduced if continuous and
autonomous condition-based damage monitoring systems can be
integrated into their design.
Therefore, development of efficient methodologies to
determine the presence, location and severity of hidden
damage in critical structural components is an important
task in the design and construction of structural health
monitoring systems in aging as well as new structures. To meet this objective, wave and vibration based
approaches are considered.
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3D Modeling and
Simulation of Guided (Lamb) Wave Propgation in Composite Plate-like
Structures:
Elastic waves
generated by foreign object impact and initiation or growth
of fatigue cracks in structural component's carry useful
information about the nature of damage associated with these
events. A clear understanding of the quantitative
relationship between the waves and their sources is
essential in developing algorithms for detecting and
characterizing the damage. Model-based analysis of the
waveform signals recorded by surface mounted or embedded
sensors located in the vicinity of the sources can lead to
the development of an effective health monitoring system for
a variety of structures.
This research is motivated by the need for an efficient and
accurate tool to analyze the wave field produced by localized
dynamic sources on the surface or the interior of
anisotropic composite laminates. A semi-analytical method
based on the wave number integral representation of the
electrodynamics field is described that reduces the overall
computational effort significantly over other available
methods. This method is used to calculate the guided
wave field produced in graphite/epoxy composite laminates by
dynamic surface loads in an effort to understand the
outstanding features of guided waves in simple plate-like
structures. The results from an approximate shear
deformation plate theory and a finite element simulation
using LSDYNA are used for model verification. The modeling and
simulation techniques are being extended to sandwich
structures for the detection of disbonds. The approach can
be used for rapid calculation of the elastic waves generated
by PZT transducers, impact sources and fatigue damage
initiation in plate-like structures, and should be useful in
providing data for NDE and SHM of critical structural
components.
Active Damage Monitoring of Structural Components Using Guided Waves:
The
current research aims to develop novel algorithms for damage
identification and localization in real-time based on
ultrasonic techniques with and without based line signals. For example, an autonomous “damage
index” approach is being developed that can provide
approximate location and severity of the damaged zone
without any visual inspection of the signals. The technique
stipulates the use of a sparsely distributed high frequency
ultrasonic sensor arrays located in critical areas to
measure the local response of a structure. Using
measurements performed on an undamaged or partially damaged
structure as baseline, the damage indices are evaluated from
the comparison of the frequency response of the monitored
structure with an unknown damage under the same ambient
conditions. Similarly, a baseline free algorithm is being developed using time-frequency analysis of the data
collected from embedded PZT arrays. Simulations are performed to
support experimental results and feature extractions for damage detection.
These techniques are applied to metallic and
composites structural components involving beams and plates
with emerging defects in the forms of impact damage, fatigue
cracks, corrosion, rivet holes etc. The relative
effectiveness of the methods is examined for a variety of
boundary conditions and sensor locations relative to the
defects.
Impact-Acoustic Emission Monitoring of Structural Composites:
Acoustic
Emission (AE) is the phenomenon in which elastic waves are
emitted from sudden release of strain energy during the
initiation and extension of cracks or other flaws in
structural solids under (fatigue or other loading). Elastic
waves are captured to extract information about the nature
of damage, and the physical mechanisms responsible for
generating the individual acoustic emission (AE) waveforms.
Hidden damage caused by foreign object impact in a composite
structure, if left undetected, can grow and lead to a
catastrophic failure of the structure. Detection of impact
events and characterization of the degree of damage caused
by them, preferably in real time, would be extremely helpful
in safe continued operation of composite structures.
The present study aims to develop a viable quantitative
impact damage monitoring tool by combining experimental,
theoretical and signal processing techniques. Low velocity
impact experiments are carried out in composite plates using
an customized impact tester and the surface motion at
locations away from the impact point is recorded using an
improved ultrasonic test-setup. It has been shown that the
occurrence of an impact loading can be easily detected from
the recorded signals. Delamination damage, if any, can also
be determined through careful analysis of the recorded
waveforms. The response of the plate due to localized
sources is calculated using an exact plate theory providing
detailed information on the relationship between the impact
load and the signals generated by the load. Practical
applications of the technique in structural health
monitoring will require careful investigation and
elimination of environmental noise.
Vibration Based Health Monitoring:
Development of
efficient methodologies to determine the presence, location,
and severity of hidden damage in critical structural
components is an important task in the design and
construction of structural health monitoring (SHM) systems
in aging as well as new structures. The traditional
non-destructive inspection (NDI) techniques such as
ultrasonic pulse-echo, radiography, thermography, etc., can
be time-consuming, costly, labour intensive and often
require disassembly of the structure, which make them
impractical and infeasible for large area inspections.
Although several global damage identification techniques
based on vibration approach are developed over the last few
decades for SHM, their actual application poses many
technical challenges. In particular, application of modal
identification techniques considering changes in natural
frequencies and mode shapes due to appearance of damage have
been found to be challenging. As a result, methods based on
the use of frequency response functions (FRFs) are developed
due to their effectiveness for reliable damage monitoring in
most applications. Thus, this research activity emphasizes
the need of a unified procedure to improve the reliability
of the defects detection capability based on FRF and aid in
the development of autonomous health monitoring systems for
defects-critical structures. The technique is being applied
in both simple structural components such as beam and plates
as well as structural frames.
Condition monitoring of concrete structures using Impact Echo simulation and measurements:
Reinforced
concrete (RC) structures are widely used in civil
infrastructure systems due to low construction cost and long
service life under various conditions. Safety of these
structures, in particular, is of paramount importance that
requires periodic inspection and maintenance. Testing of
thick concrete structures using ultrasonic pulse-echo
technique is often difficult due to heavy scattering and
attenuation of the sound energy in the medium. Impact-Echo
Technique is therefore often utilized for inspections of
thicker components. Research activities encompass
development of techniques based on simulated and
experimental data for rapid inspections of these structures
to identify variety of defects. |
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Computational Design of Ultrastong Nano-layered Materials
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Recent developments in Nanotechnology has opened up new
possibilities to design new ultra strong and yet ductile
materials by combining nanolayers with different
microstructures. Such materials have potential applications
in many areas, e.g. microelectronics, optoelectronics,
aircraft structures, rocket engines and fuel cells.
Development of such materials requires a detail
understanding of their mechanical properties. Undoubtedly,
defects (dislocations) are expected to play a key role on
the physical and mechanical performance of nano/micro-engineered
devices. Thus, multiscale material modeling (MMM) approaches
for computational materials designs are playing an ever
increasing role in this area to ensure high level of
reliability and useful lifetimes, and to reduce development
costs and manufacturing times [1].
[1] Ghoniem, N. M., Huang, H., Busso, E. and Kioussis, N.,
'Multiscale Modeling of Nano- and Micro-Mechanics: An
Overview,' Philosophical Magazine A, 83 (31-34), 3475–3528,
2003.
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Atomistic-continuum
Modeling Approach:
A newly developed, numerically stable, and robust approach
has been used to represent a wide variety of defects in
three-dimensional space, spanning from the nanoscale to the
macroscopic size. This approach bases the computational
differential geometry of the defect on the so-called
parametric dislocation dynamics (PDD), combined with local
atomistic forces based on ab initio methods, to resolve the
elastic field and the energies resulting from the defect.
The method mainly accounts for a balance between the elastic
forces due to long-range interactions among the dislocations
(using elastostatic Green’s function), the curvature of the
dislocation itself, applied force, and the local atomistic
forces. The high displacement gradients (or discontinuities)
across defect surfaces are represented by distributions of
dislocations, whose shape is determined by differential
geometry. The marriage of the continuum and atomistic
treatments combines the strength of each component and
represents an important step towards the grand goal of
'putting chemistry into mechanics'. The hybrid method deals
with the long-range elastic interactions via the continuum PDD method, and retains the atomic details only at the
dislocation core with the help of an ab initio-determined
GSF energy (gamma) surface – thus offering a computationally
effective method of minimal commitment to atomic details and
removing the long-standing problem of singularities
intrinsic to the classical continuum theory of dislocations.
This allows the prediction of nano-scale description of the
dislocation structure in more realistic geometry and
conditions (e.g. loop nucleation from crack tips or
penetrating interfaces between anisotropic nono-layers,
etc., which, in turn, determines the maximum strength) and
offers a computationally effective method of minimal
commitment to atomic details.
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