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    <title>DSpace Collection: Thesis published in Dept. of Mathematics</title>
    <link>http://103.99.128.19:8080/xmlui/handle/123456789/124</link>
    <description>Thesis published in Dept. of Mathematics</description>
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        <rdf:li rdf:resource="http://103.99.128.19:8080/xmlui/handle/123456789/602" />
        <rdf:li rdf:resource="http://103.99.128.19:8080/xmlui/handle/123456789/599" />
        <rdf:li rdf:resource="http://103.99.128.19:8080/xmlui/handle/123456789/589" />
        <rdf:li rdf:resource="http://103.99.128.19:8080/xmlui/handle/123456789/567" />
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    <dc:date>2026-10-05T08:47:52Z</dc:date>
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  <item rdf:about="http://103.99.128.19:8080/xmlui/handle/123456789/602">
    <title>SIMULATION OF HEAT TRANSFER  ENHANCEMENT IN A PIPE USING RECTANGULAR  CUT TWISTED TAPE INSERT: A FEM APPROACH</title>
    <link>http://103.99.128.19:8080/xmlui/handle/123456789/602</link>
    <description>Title: SIMULATION OF HEAT TRANSFER  ENHANCEMENT IN A PIPE USING RECTANGULAR  CUT TWISTED TAPE INSERT: A FEM APPROACH
Authors: Anika, Onamika Ibnath; ID :, 21MMATH009F
Abstract: A simulation analysis has been conducted to investigate heat transfer enhancement &#xD;
using rectangular-cut twisted tape inserts in a U-shaped pipe. Numerical simulations &#xD;
have also been carried out for a plain tube and a tube with smooth twisted tape (TT) &#xD;
inserts, and the results have been compared across three configurations: rectangular-cut &#xD;
TT inserts, smooth TT inserts, and the plain tube. The analysis has utilized a U-bend &#xD;
pipe with a length of 1935.6 mm and an inner diameter of 26.6 mm. For non-isothermal &#xD;
turbulent flow, water has been selected as the working fluid, and the Reynolds number &#xD;
(Re) range has been considered from 5319.4 to 17288.05. The rectangular-cut twisted &#xD;
tape inserts have demonstrated superior heat transfer performance compared to the other &#xD;
two configurations due to enhanced fluid mixing in the turbulent flow regime. In this &#xD;
study, the dimensionless Nusselt number (Nu) has consistently been higher for the &#xD;
rectangular-cut twisted tape configuration and has shown a gradual increase with rising &#xD;
Reynolds numbers. The results have also indicated improved thermal performance (ɳ), &#xD;
with a thermal performance factor of 1.04 and favorable friction factor values for the &#xD;
pipe fitted with rectangular cut twisted tape inserts.
Description: A Master of Philosophy (M.Phil.) Thesis in Mathematics  Department at Chittagong University of Engineering and Technology (CUET).</description>
    <dc:date>2025-04-08T00:00:00Z</dc:date>
  </item>
  <item rdf:about="http://103.99.128.19:8080/xmlui/handle/123456789/599">
    <title>NUMERICAL INVESTIGATIONOFNONLINEAR ACOUSTICWAVEPHENOMENA INSTRONGLYAND WEAKLYCOUPLEDPLASMAS</title>
    <link>http://103.99.128.19:8080/xmlui/handle/123456789/599</link>
    <description>Title: NUMERICAL INVESTIGATIONOFNONLINEAR ACOUSTICWAVEPHENOMENA INSTRONGLYAND WEAKLYCOUPLEDPLASMAS
Authors: Islam, Md. Nazrul
Abstract: This thesis investigates nonlinear acoustic wave phenomena in both strongly and weakly&#xD;
coupled collisionless unmagnetized plasmas using analytical and numerical methods. By&#xD;
developing mathematical models for different plasma environments, the study employs the&#xD;
reductive perturbation technique (RPT) to derive nonlinear evolution equations (NLEEs).&#xD;
These equations are then used to analyze the propagation of shock waves, solitons, and&#xD;
periodic waves in various plasma configurations.&#xD;
In Chapter 2, Burgers equations involving quadratic, cubic, and combined&#xD;
quadratic-cubic nonlinearities are derived for a coupled complex plasma system consisting&#xD;
of Boltzmann-distributed electrons, nonthermal ions, and charged dust particles. The&#xD;
generalized Riccati equation mapping method (GREMM) is employed to obtain both shock&#xD;
and oscillatory wave solutions from these equations, while parametric effects on wave&#xD;
characteristics are systematically examined.&#xD;
Chapter 3 investigates heavy ion-acoustic shock waves (HIASWs) in a plasma&#xD;
comprising inertial heavy ions, Maxwellian light ions, and (α,q)-distributed electrons, by&#xD;
deriving the Burgers, modified Burgers, and mixed modified Burgers equations. The study&#xD;
presents stationary shock wave solutions for these equations and examines how plasma&#xD;
parameters influence shock wave characteristics.&#xD;
Chapter 4 investigates the dust acoustic (DA) shock wave phenomena in an strongly&#xD;
coupled dusty plasma. By deriving Burgers equations with quadratic, cubic, and quartic&#xD;
nonlinearities, we analyze shock wave behavior near critical values (CVs) and super-critical&#xD;
values (SCVs), revealing how polarization force and coupling parameter modifies shock&#xD;
wave excitations.&#xD;
Chapter 5 analyzes heavy ion-acoustic (HIA) solitons and dressed solitons in&#xD;
weakly/strongly coupled plasmas with nonthermal electrons.&#xD;
Chapter 6 advances the Chapter 3 framework by examining HIASWs near CVs and&#xD;
SCVs, deriving a non-integrable NLEE with combined cubic-quartic nonlinearities that&#xD;
necessitates numerical solution via Runge-Kutta-Fehlberg analysis.&#xD;
Thus, the thesis enhances understanding of nonlinear coherent structures observed in&#xD;
various space and astrophysical environments.
Description: A Doctor of Philosophy (Ph.D.) Thesis in Mathematics Department at Chittagong University of Engineering and Technology (CUET).</description>
    <dc:date>2025-07-17T00:00:00Z</dc:date>
  </item>
  <item rdf:about="http://103.99.128.19:8080/xmlui/handle/123456789/589">
    <title>DESIGNING CONTROL SCHEMS FOR  CHAOTIC SYSTEMS VIA SLIDING  MODE CONTROL</title>
    <link>http://103.99.128.19:8080/xmlui/handle/123456789/589</link>
    <description>Title: DESIGNING CONTROL SCHEMS FOR  CHAOTIC SYSTEMS VIA SLIDING  MODE CONTROL
Authors: AFROJA, AFSANA; ID:, 21MMATH002P
Abstract: Among various robust control methods, Sliding Mode Control (SMC) has attracted &#xD;
considerable interest in theoretical research due to its unique features. SMC is well known &#xD;
for its robustness to matched and bounded uncertainties, reduction in the order of the &#xD;
system during the sliding phase, simplified decoupling of system dynamics, and its ability &#xD;
to achieve zero steady-state error. These characteristics make SMC a powerful tool in &#xD;
designing control systems for uncertain and nonlinear environments. &#xD;
This thesis presents a comprehensive study on the control and synchronization of chaotic &#xD;
systems, focusing on the Modified Lorenz System (MLS) and the Liu financial dynamical &#xD;
system. Chaotic behavior, with its sensitivity to initial conditions, presents major &#xD;
challenges in nonlinear control. Sliding Mode Control (SMC) is applied to coupled MLS &#xD;
to ensure robust synchronization through a designed sliding surface and control law, with &#xD;
convergence proven via Lyapunov stability and validated through numerical simulations. &#xD;
In the Liu financial system, both SMC and Passive Control (PC) are implemented and &#xD;
compared. While SMC provides rapid synchronization (within 𝑡 ≥ 1, error reduced from &#xD;
5.67 to 0.02), PC achieves synchronization more gradually (within 𝑡 ≤ 13, error reduced &#xD;
from 6.21 to 0.03) using a simpler, single-controller strategy. The results highlight key &#xD;
trade-offs between speed, robustness, and implementation complexity, offering valuable &#xD;
insights into managing chaos in nonlinear and financial systems. &#xD;
These limitations have motivated ongoing research aimed at improving SMC design. The &#xD;
core challenge remains how to develop a simple yet effective sliding mode control &#xD;
technique that retains its robustness and zero-error tracking while minimizing chattering &#xD;
and relaxing the need for precise uncertainty bounds.
Description: A Master of Philosophy (M.Phil.) Thesis in Mathematics  Department at Chittagong University of Engineering and Technology (CUET).</description>
    <dc:date>2025-07-07T00:00:00Z</dc:date>
  </item>
  <item rdf:about="http://103.99.128.19:8080/xmlui/handle/123456789/567">
    <title>ISOTROPIC SOLUTION OF EINSTEIN’S EQUATIONS ONTHE FLUIDSPHERE</title>
    <link>http://103.99.128.19:8080/xmlui/handle/123456789/567</link>
    <description>Title: ISOTROPIC SOLUTION OF EINSTEIN’S EQUATIONS ONTHE FLUIDSPHERE
Authors: HOSSAIN, MD.IMRAN; ID:, 21MMATH005
Abstract: This thesis investigates the theoretical framework of spherically symmetric perfect&#xD;
fluid spheres within the realm of general relativity. Our work seeks exact solutions to the&#xD;
Einstein field equations thereby facilitating a better knowledge of minuscule objects. The&#xD;
thesis begins by examining the fundamental aspects of special relativity, including the&#xD;
Lorentz transformations and the structure of spacetime. We then explore general relativity,&#xD;
with an eye towards the Einstein field equations and the geometric justification of gravity.&#xD;
Examining matter dispersion in astrophysical systems depends on first looking at the&#xD;
behavior of ideal fluids.&#xD;
The thesis delves into the intricacies of the Einstein field equations and their application&#xD;
to spacetimes with spherical symmetry. The key achievement of the research is the&#xD;
formulation of new exact solutions for static spherically symmetric ideal fluid spheres.&#xD;
Implementing two techniques in the context of static spherically symmetric ideal fluid line&#xD;
elements, we develop two new approaches that validate their characteristics and ensure&#xD;
that they satisfy Buchdhal criteria.&#xD;
The physical characteristics and possible astrophysical implications of these solutions are&#xD;
thoroughly investigated. Combining the ideas of general relativity with the simplified&#xD;
model of perfect fluids helps this work provide new understanding on the interactions&#xD;
between compact objects and their gravitational interactions.
Description: An M.Phil. Thesis in Mathematics Department at Chittagong University of Engineering and Technology (CUET).</description>
    <dc:date>2025-03-20T00:00:00Z</dc:date>
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