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<title>Master's Thesis</title>
<link>http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/66</link>
<description/>
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<rdf:li rdf:resource="http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/1041"/>
<rdf:li rdf:resource="http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/820"/>
<rdf:li rdf:resource="http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/790"/>
<rdf:li rdf:resource="http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/664"/>
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<dc:date>2026-04-22T13:28:57Z</dc:date>
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<item rdf:about="http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/1041">
<title>DEVELOPMENT OF A DIVER PROPULSION VEHICLE SIMULATOR FOR SEARCH AND RESCUE OPERATION</title>
<link>http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/1041</link>
<description>DEVELOPMENT OF A DIVER PROPULSION VEHICLE SIMULATOR FOR SEARCH AND RESCUE OPERATION
NAZMUL HAQ, MOHAMMED
Diver Propulsion Vehicle (DPV) is a self-propelled device used to facilitate divers to move &#13;
freely underwater for search and rescue operations as well as for exploration purposes. DPV &#13;
provides speed and a long-range to cover a wide area for various diving operations. A DPV &#13;
generally consists of a pressure-resistant waterproof casing with a battery-powered electric &#13;
motor that drives the propeller. It is  widely used across the globe very effectively with a &#13;
varying range of design and endurance capabilities. The design and fabrication of DPVs &#13;
have been done in many developed countries. Indigenous design and fabrication of DPV &#13;
are possible by utilizing local resources of Bangladesh. Designed prototype DPV is &#13;
developed using SolidWorks, and a CFD analysis is carried out using Ansys software. After &#13;
that, a DPV model is fabricated using resources from the local market. This project &#13;
preliminarily focused on design, fabrication of DPV and simulated various parameters to &#13;
get better results. Finally, the test and trial results and performance of the DPV are &#13;
evaluated so that it can be used effectively for search and rescue operations in Bangladesh.
Development of A Diver Propulsion Vehicle Simulator for Search and Rescue &#13;
Operation
</description>
<dc:date>2023-06-01T00:00:00Z</dc:date>
</item>
<item rdf:about="http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/820">
<title>FABRICATION AND PERFORMANCE EVALUATION OF LOW COST HIGH IMPACT RESISTANT COMPOSITE</title>
<link>http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/820</link>
<description>FABRICATION AND PERFORMANCE EVALUATION OF LOW COST HIGH IMPACT RESISTANT COMPOSITE
RAHMAN, MD. ANISUR
In this thesis low cost composite laminates were fabricated and their effectiveness against&#13;
high impact was assessed. Glass fiber was used as the fiber and epoxy resin as the binder&#13;
to create composite laminates. For enhanced binding properties, hardener and 6% cobalt&#13;
were additionally included with the binder. The laminates vary in terms of layer count,&#13;
glass fiber type (woven or matt), and curing time. For better comparison between same&#13;
type of laminates, a few more variables, including the percentage of hardener, the&#13;
quantity of matrix, and the curing time, were held constant. The mechanical properties&#13;
were measured giving the Impact test more importance. The mechanical property tests&#13;
such as the tensile test, compression test, bending test, Charpy impact test, Izod test, and&#13;
free fall impact tests were done according to the different standardized test method. A&#13;
laminate with greater performance was found after comparing all the attributes. The&#13;
production costs were successfully reduced by the thesis because all the materials were&#13;
readily available and locally manufactured with simple setups. The thesis successfully&#13;
suggested a possible low-cost production setup for high impact resistant materials.
The author firstly thanks Almighty Allah for His relentless blessings to complete this&#13;
thesis work. The author would like to thank Professor Dr. Afsar Ali, who oversaw his&#13;
thesis, for his advice, support, and assistance with this study work. The author would like&#13;
to thank his co-supervisor, Prof. Dr. Enamul Hoque, for his consistent oversight,&#13;
passionate observations, and direction throughout the thesis. The department's Dean, Brig&#13;
Gen Md Humayun Kabir Bhuiyan, psc, whose guidance and support allowed the author to&#13;
labor tirelessly and introduce new ideas, is also noteworthy. The author would also like to&#13;
recognize the efforts of the lab staff, in particular Sub Asst Engr Mr. Md. Raju Ahmed&#13;
and Sub Asst Engr Mr. Dibakar Tarafdar, who assisted with the setup and execution of&#13;
experiments for the research work. Last but not the least, the author would like to express&#13;
his utmost gratitude to his family members who has been patient and supportive all&#13;
through this journey.
</description>
<dc:date>2023-03-01T00:00:00Z</dc:date>
</item>
<item rdf:about="http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/790">
<title>ANALYSIS OF MAGNETIC FIELD EFFECT ON PULSATING BLOOD FLOW IN ARTERIES</title>
<link>http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/790</link>
<description>ANALYSIS OF MAGNETIC FIELD EFFECT ON PULSATING BLOOD FLOW IN ARTERIES
OISHE, SADIA NOON
Cardiovascular diseases including strokes, heart attacks, Stenosis, and atherosclerosis are&#13;
considered the leading cause of death over the globe. The aorta, coronary, carotid, and&#13;
femoral arteries are the most commonly impacted arteries. It's a crucial field of study for&#13;
blood flow behavior. For many years, researchers have experimented with various&#13;
numerical strategies to entice clinicians to trust their colorful contours. In recent, the impact&#13;
of magnetic fields on blood flow is one of the developing approaches to treating different&#13;
types of diseases. However, the efficiency of MHD capture is still unclear, and there is less&#13;
systematic strategy to understand the flow behavior of blood. In this study, a simulationbased three-dimensional human aorta (brachiocephalic trunk, left subclavian, and left&#13;
carotid) with transient conditions is analyzed to predict changes in blood flow distribution&#13;
and flow patterns under with and without magnetic field conditions. Blood is modeled as&#13;
non-Newtonian fluids along with plasma. VOF modeling for multiphase flow is used to&#13;
mix RBC and plasma to predict the pulsating condition for the flow. Moreover, 1 Tesla&#13;
magnetic field is applied to the selected section of the aorta. For simulation purposes,&#13;
ANSYS Fluent software is used to identify the values for velocity, pressure, and wall shear&#13;
force to understand the flow behavior of blood. The result shows that velocity, pressure,&#13;
and wall shear stress are affected by exposure to MHD. By applying MHD, due to the&#13;
freezing effect, the flow velocity slows down by about .035% while pressure increases by&#13;
9%, wall shear stress increases by 1.46% as well as mass flow.
All praise be to Allah, the Cherisher and Sustainer of the worlds for His kindness and&#13;
blessings for allowing me to do this colossal work and finally materialize it.&#13;
The author expresses her deepest gratitude and profound indebtedness to her supervisor,&#13;
Professor Dr. Dipak Kanti Das, Department of Mechanical Engineering, MIST, Dhaka, for&#13;
his continuous supervision, valuable opinions, and motivation for research work all through&#13;
the time. His regular support and direction made this research work possible and fruitful at&#13;
every stage.&#13;
The author is also thankful to Brig Gen Md Humayun Kabir Bhuiyan, psc, Dean,&#13;
Department of Mechanical Engineering, MIST for his encouragement throughout the&#13;
whole course. Special gratitude to Brig Gen Md. Omar Faruque, afwc, psc, Head,&#13;
Department of Mechanical Engineering, MIST for his guidance at every step is duly&#13;
acknowledged. The author would also like to thank Professor Dr. R. G. M Hasan for&#13;
supporting me academically and personally and Professor Dr. A.B.M. Toufique Hasan for&#13;
his valuable guidance and thanks to all Department of Mechanical Engineering, MIST for&#13;
their cooperation in the successful fulfillment of the work.&#13;
Finally, the author would like to express sincere thanks to all the beautiful people who&#13;
stayed beside them when truly needed their support for the successful completion of this&#13;
work.
</description>
<dc:date>2022-04-01T00:00:00Z</dc:date>
</item>
<item rdf:about="http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/664">
<title>Numerical and Experimental Investigation of Non-Circular Free Jet with and without Peripheral Twist for Improvement in Mass Entrainment, Mixing and Turbulence Characteristics</title>
<link>http://dspace.mist.ac.bd:8080/xmlui/handle/123456789/664</link>
<description>Numerical and Experimental Investigation of Non-Circular Free Jet with and without Peripheral Twist for Improvement in Mass Entrainment, Mixing and Turbulence Characteristics
Rahman Evan, Md.Touhidur
Free jet flow is a basic flow configuration found in wide range of applications,&#13;
majority of them being mixing, heating or cooling. The present study is therefore focused&#13;
to improve the performance of the free turbulent jets within its ‘developing zone’ using&#13;
two different mechanisms viz. (a) use of non-circular cross section jet and (b)&#13;
introduction of swirl to jet by means of peripheral twist. The present research considers&#13;
experimental and computational study of circular and non-circular turbulent jets (having&#13;
Reynolds number 7.2 ×104 based on jet exit diameter). A ‘jet modifier pipe’, is used for&#13;
the creation of circular and non-circular jets. Essentially, jet modifier pipe is small pipe&#13;
through which circular jet is gradually changed to non-circular jet. Axial center line&#13;
velocity, jet spread rate, potential core length and jet velocity profiles at various&#13;
downstream locations are measured both experimentally and computationally.&#13;
Turbulence intensity and tangential velocities at different downstream locations of the&#13;
jet are determined numerically.&#13;
The comparison of local jet velocity along jet axis indicates that the deceleration&#13;
of axial velocity for triangular jet is maximum while that for circular jet is minimum&#13;
which is indicating maximum potential core length for circular jet. A consistent&#13;
observation is also showcased by jets wherein, the potential core length for circular jet is&#13;
maximum, while non-circular jets show lower core length. The peak turbulence intensity&#13;
location is found closer to jet exit for triangular and rectangular jets which is an indicator&#13;
of efficient mixing. Rectangular jets show saddle shape profile at downstream of the pipe&#13;
exit. The rectangular jet possesses an upper hand in terms of jet performance&#13;
characteristics from the point of mixing characteristics.&#13;
In order to improve the mixing characteristics of non-circular jets, a peripheral&#13;
twist has been provided to jet modifier pipe. The parametric analysis included study of&#13;
twist rate and length of jet modifier pipe. The study indicates that, increase in twist rate&#13;
of jet modifier pipe increases tangential velocity of jet, with rectangular jet outperforming&#13;
square and triangular jets. The twisted jet modifier pipe length has an opposite effect&#13;
wherein, the smaller the length of pipe, the higher is the tangential velocity. In nut shell&#13;
the computational and experimental studies indicate that the peripheral twist introduced&#13;
to non-circular free jets are far superior to the circular free jet in the mixing process.
</description>
<dc:date>2018-12-01T00:00:00Z</dc:date>
</item>
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