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This book discusses systems of damage detection and structural
health monitoring in mechanical, civil, and aerospace structures.
It utilizes principles of fuzzy logic, probability theory, and
signal processing to develop systems and approaches that are robust
in the presence of both noise in the data and variations in
properties of materials which are intrinsic to the process of mass
production. This volume will be useful to graduate students,
researchers, and engineers working in this area, especially those
looking to understand and address model uncertainty in their
algorithms.
The book addresses computational methods for solving the problem of
vibration, response, loads and stability of a helicopter rotor
blade modeled as a rotating beam with flap or out-of-plane bending.
The focus is on explaining the implementation of the finite element
method in the space and time domain for the free vibration,
aeroelastic response and stability problems. The use of Floquet
analysis for the aeroelastic stability analysis of rotor blades is
also shown. The contents of the book will be useful to researchers
in aerodynamics and applied mechanics, and will also serve well
professionals working in the aerospace industry.
Exploiting the properties of piezoelectric materials to minimize
vibration in rotor-blade actuators, this book demonstrates the
potential of smart helicopter rotors to achieve the smoothness of
ride associated with jet-engined, fixed-wing aircraft. Vibration
control is effected using the concepts of trailing-edge flaps and
active-twist. The authors' optimization-based approach shows the
advantage of multiple trailing-edge flaps and algorithms for
full-authority control of dual trailing-edge-flap actuators are
presented. Hysteresis nonlinearity in piezoelectric stack actuators
is highlighted and compensated by use of another algorithm. The
idea of response surfaces provides for optimal placement of
trailing-edge flaps. The concept of active twist involves the
employment of piezoelectrically induced shear actuation in rotating
beams. Shear is then demonstrated for a thin-walled
aerofoil-section rotor blade under feedback-control vibration
minimization. Active twist is shown to be significant in reducing
vibration caused by dynamic stall. The exposition of ideas,
materials and algorithms in this monograph is supported by
extensive reporting of results from numerical simulations of smart
helicopter rotors. This monograph will be a valuable source of
reference for researchers and engineers with backgrounds in
aerospace, mechanical and electrical engineering interested in
smart materials and vibration control. Advances in Industrial
Control aims to report and encourage the transfer of technology in
control engineering. The rapid development of control technology
has an impact on all areas of the control discipline. The series
offers an opportunity for researchers to present an extended
exposition of new work in all aspects of industrial control.
This book presents an isospectral approach for several important
mechanical vibrating systems. Discrete and continuous isospectral
systems are discussed using a simple multi-degree of freedom
spring-mass system followed by illustration of isospectral beams
and their solution through evolutionary computing. Next, it
addresses axially loaded Euler-Bernoulli beams and aims to find
isospectral counterparts of these systems. The practical
application of these isospectral systems for vibration testing and
for finding new closed form solutions is discussed. A considerable
part of the book is devoted to isospectral rotating beams and their
non-rotating analogs including Rayleigh beams. Aimed at researchers
and graduate students in mechanical; aerospace; civil; automotive;
ocean engineering especially mechanical vibrations, this monograph:
Discusses isospectral vibrating systems to aid vibration testing
and computational analysis Explores isospectral analogs between
rotating and non-rotating structures Provides simpler isospectral
beams for vibration testing and for 3D printing Uses firefly
optimization method and electromagnetism inspired optimization
method to find isospectral systems Shows the use of isospectral
systems to find new closed form solutions using an indirect
approach
Provides background material needed to understand digital twin
technology Presents computational facet of digital twin Includes
physics based and surrogate model representations Addresses the
problem of uncertainty in measurements and modeling Discusses
practical case studies of implementation of digital twins
addressing additive manufacturing, server farms, predictive
maintenance, and smart cities
Structural health monitoring (SHM) has emerged as a prominent
research area in recent years owing to increasing concerns about
structural safety, and the need to monitor and extend the lives of
existing structures. Structural Health Monitoring Using Genetic
Fuzzy Systems elaborates the process of intelligent SHM development
and implementation using the evolutionary system. The use of a
genetic algorithm automates the development of the fuzzy system,
and makes the method easy to use for problems involving a large
number of measurements, damage locations and sizes; such problems
being typical of SHM. The ideas behind fuzzy logic, genetic
algorithms and genetic fuzzy systems are also explained. The
functionality of the genetic fuzzy system architecture is
elucidated within a case-study framework, covering: * SHM of beams;
* SHM of composite tubes; and * SHM of helicopter rotor blades.
Structural Health Monitoring Using Genetic Fuzzy Systems will be
useful for aerospace, civil and mechanical engineers working with
structures and structured components. It will also be useful for
computer scientists and applied mathematicians interested in the
application of genetic fuzzy systems to engineering problems.
This book presents an isospectral approach for several important
mechanical vibrating systems. Discrete and continuous isospectral
systems are discussed using a simple multi-degree of freedom
spring-mass system followed by illustration of isospectral beams
and their solution through evolutionary computing. Next, it
addresses axially loaded Euler-Bernoulli beams and aims to find
isospectral counterparts of these systems. The practical
application of these isospectral systems for vibration testing and
for finding new closed form solutions is discussed. A considerable
part of the book is devoted to isospectral rotating beams and their
non-rotating analogs including Rayleigh beams. Aimed at researchers
and graduate students in mechanical; aerospace; civil; automotive;
ocean engineering especially mechanical vibrations, this monograph:
Discusses isospectral vibrating systems to aid vibration testing
and computational analysis Explores isospectral analogs between
rotating and non-rotating structures Provides simpler isospectral
beams for vibration testing and for 3D printing Uses firefly
optimization method and electromagnetism inspired optimization
method to find isospectral systems Shows the use of isospectral
systems to find new closed form solutions using an indirect
approach
Widely used for power generation, gas turbine engines are
susceptible to faults due to the harsh working environment. Most
engine problems are preceded by a sharp change in measurement
deviations compared to a baseline engine, but the trend data of
these deviations over time are contaminated with noise and
non-Gaussian outliers. Gas Turbine Diagnostics: Signal Processing
and Fault Isolation presents signal processing algorithms to
improve fault diagnosis in gas turbine engines, particularly jet
engines. The algorithms focus on removing noise and outliers while
keeping the key signal features that may indicate a fault. The book
brings together recent methods in data filtering, trend shift
detection, and fault isolation, including several novel approaches
proposed by the author. Each method is demonstrated through
numerical simulations that can be easily performed by the reader.
Coverage includes: Filters for gas turbines with slow data
availability Hybrid filters for engines equipped with faster data
monitoring systems Nonlinear myriad filters for cases where
monitoring of transient data can lead to better fault detection
Innovative nonlinear filters for data cleaning developed using
optimization methods An edge detector based on gradient and
Laplacian calculations A process of automating fault isolation
using a bank of Kalman filters, fuzzy logic systems, neural
networks, and genetic fuzzy systems when an engine model is
available An example of vibration-based diagnostics for turbine
blades to complement the performance-based methods Using simple
examples, the book describes new research tools to more effectively
isolate faults in gas turbine engines. These algorithms may also be
useful for condition and health monitoring in other systems where
sharp changes in measurement data indicate the onset of a fault.
This book discusses systems of damage detection and structural
health monitoring in mechanical, civil, and aerospace structures.
It utilizes principles of fuzzy logic, probability theory, and
signal processing to develop systems and approaches that are robust
in the presence of both noise in the data and variations in
properties of materials which are intrinsic to the process of mass
production. This volume will be useful to graduate students,
researchers, and engineers working in this area, especially those
looking to understand and address model uncertainty in their
algorithms.
Structural health monitoring (SHM) has emerged as a prominent
research area in recent years owing to increasing concerns about
structural safety, and the need to monitor and extend the lives of
existing structures. Structural Health Monitoring Using Genetic
Fuzzy Systems elaborates the process of intelligent SHM development
and implementation using the evolutionary system. The use of a
genetic algorithm automates the development of the fuzzy system,
and makes the method easy to use for problems involving a large
number of measurements, damage locations and sizes; such problems
being typical of SHM. The ideas behind fuzzy logic, genetic
algorithms and genetic fuzzy systems are also explained. The
functionality of the genetic fuzzy system architecture is
elucidated within a case-study framework, covering: * SHM of beams;
* SHM of composite tubes; and * SHM of helicopter rotor blades.
Structural Health Monitoring Using Genetic Fuzzy Systems will be
useful for aerospace, civil and mechanical engineers working with
structures and structured components. It will also be useful for
computer scientists and applied mathematicians interested in the
application of genetic fuzzy systems to engineering problems.
Widely used for power generation, gas turbine engines are
susceptible to faults due to the harsh working environment. Most
engine problems are preceded by a sharp change in measurement
deviations compared to a baseline engine, but the trend data of
these deviations over time are contaminated with noise and
non-Gaussian outliers. Gas Turbine Diagnostics: Signal Processing
and Fault Isolation presents signal processing algorithms to
improve fault diagnosis in gas turbine engines, particularly jet
engines. The algorithms focus on removing noise and outliers while
keeping the key signal features that may indicate a fault. The book
brings together recent methods in data filtering, trend shift
detection, and fault isolation, including several novel approaches
proposed by the author. Each method is demonstrated through
numerical simulations that can be easily performed by the reader.
Coverage includes: Filters for gas turbines with slow data
availability Hybrid filters for engines equipped with faster data
monitoring systems Nonlinear myriad filters for cases where
monitoring of transient data can lead to better fault detection
Innovative nonlinear filters for data cleaning developed using
optimization methods An edge detector based on gradient and
Laplacian calculations A process of automating fault isolation
using a bank of Kalman filters, fuzzy logic systems, neural
networks, and genetic fuzzy systems when an engine model is
available An example of vibration-based diagnostics for turbine
blades to complement the performance-based methods Using simple
examples, the book describes new research tools to more effectively
isolate faults in gas turbine engines. These algorithms may also be
useful for condition and health monitoring in other systems where
sharp changes in measurement data indicate the onset of a fault.
Exploiting the properties of piezoelectric materials to minimize
vibration in rotor-blade actuators, this book demonstrates the
potential of smart helicopter rotors to achieve the smoothness of
ride associated with jet-engined, fixed-wing aircraft. Vibration
control is effected using the concepts of trailing-edge flaps and
active-twist. The authors' optimization-based approach shows the
advantage of multiple trailing-edge flaps and algorithms for
full-authority control of dual trailing-edge-flap actuators are
presented. Hysteresis nonlinearity in piezoelectric stack actuators
is highlighted and compensated by use of another algorithm. The
idea of response surfaces provides for optimal placement of
trailing-edge flaps. The concept of active twist involves the
employment of piezoelectrically induced shear actuation in rotating
beams. Shear is then demonstrated for a thin-walled
aerofoil-section rotor blade under feedback-control vibration
minimization. Active twist is shown to be significant in reducing
vibration caused by dynamic stall. The exposition of ideas,
materials and algorithms in this monograph is supported by
extensive reporting of results from numerical simulations of smart
helicopter rotors. This monograph will be a valuable source of
reference for researchers and engineers with backgrounds in
aerospace, mechanical and electrical engineering interested in
smart materials and vibration control. Advances in Industrial
Control aims to report and encourage the transfer of technology in
control engineering. The rapid development of control technology
has an impact on all areas of the control discipline. The series
offers an opportunity for researchers to present an extended
exposition of new work in all aspects of industrial control.
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