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  <title>DSpace Community:</title>
  <link rel="alternate" href="http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/132" />
  <subtitle />
  <id>http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/132</id>
  <updated>2026-04-14T11:08:21Z</updated>
  <dc:date>2026-04-14T11:08:21Z</dc:date>
  <entry>
    <title>Understanding the Force Deflection Behavior of NiTi  Archwire at Distinct Bending Configuration: A  Narrative Review in Vitro Studies</title>
    <link rel="alternate" href="http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/11809" />
    <author>
      <name>Munir, A</name>
    </author>
    <author>
      <name>Zulfiqar, S</name>
    </author>
    <author>
      <name>Joy Mathavan, J.</name>
    </author>
    <author>
      <name>Sohail, A</name>
    </author>
    <id>http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/11809</id>
    <updated>2025-11-24T08:59:32Z</updated>
    <published>2024-01-01T00:00:00Z</published>
    <summary type="text">Title: Understanding the Force Deflection Behavior of NiTi  Archwire at Distinct Bending Configuration: A  Narrative Review in Vitro Studies
Authors: Munir, A; Zulfiqar, S; Joy Mathavan, J.; Sohail, A
Abstract: This study aims to assess the optimal unloading force range for human comfort &#xD;
by considering NiTi archwires in different bending settings, based on previous research &#xD;
findings. All the relative data has been collected from different databases such as PubMed, &#xD;
Google Scholar, Scopus, Web of Science, and USM library. The publications from 2007 till &#xD;
February 2023 have been incorporated. Several parameters related to orthodontics, &#xD;
especially the usage of three brackets and three-point bending with respect to optimal tooth &#xD;
force were taken into consideration. These parameters, however, included various aspects &#xD;
like the shape memory effect, bending temperature, friction, and gingival/labial direction. &#xD;
ISO standards pertaining to the bending tests were also contemplated in this review. The &#xD;
study examined 74 articles related to orthodontic tooth movement, three brackets, and &#xD;
three-point bending. In fact, this review was done to analyze the force deflection behavior &#xD;
and related parameters to orthodontics. For this, among 74 selected research items, 15 &#xD;
studies gave information about the optimal tooth force, 8 focused on the optimal ranges, &#xD;
while 7 reports indicated the higher rates of tooth force. All these studies illustrated the &#xD;
considerable variation in methodology and clinical diversity in terms of applied forces. This &#xD;
article summarizes previous investigations on orthodontic tooth force, highlighting the ideal &#xD;
range of 0.2 to 1.5 N. It concludes that maximum force decreases with greater inter-bracket &#xD;
distance but increases with wire deflection and testing temperature. Proper force &#xD;
management is emphasized as crucial for preventing unwanted tooth movement and its &#xD;
biological consequences.</summary>
    <dc:date>2024-01-01T00:00:00Z</dc:date>
  </entry>
  <entry>
    <title>SELF-NAVIGATION INTERFACE SYSTEM IN COMPLEX BUILDINGS USING  MICROCONTROLLER</title>
    <link rel="alternate" href="http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/11808" />
    <author>
      <name>Raafeek, A.R.M</name>
    </author>
    <author>
      <name>Kunaraj, A.</name>
    </author>
    <author>
      <name>Joy Mathavan, J.</name>
    </author>
    <id>http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/11808</id>
    <updated>2025-11-24T09:03:26Z</updated>
    <published>2024-01-01T00:00:00Z</published>
    <summary type="text">Title: SELF-NAVIGATION INTERFACE SYSTEM IN COMPLEX BUILDINGS USING  MICROCONTROLLER
Authors: Raafeek, A.R.M; Kunaraj, A.; Joy Mathavan, J.
Abstract: Self-navigation technology proves to be among the most advanced methods &#xD;
for locating specific positions. However, it remains challenging to accurately determine &#xD;
desired locations within intricate building structures using self-navigation. This research &#xD;
introduces a cutting-edge Self-Navigation and Interface System designed to address the &#xD;
complexities of indoor navigation in diverse environments such as universities, banks, &#xD;
shopping centres, and restaurants. The system leverages microcontroller technology as its &#xD;
control system, featuring a bespoke app interface integrated with microcontroller and &#xD;
Bluetooth modules. The app, accessible via system-installed touchscreens or mobile &#xD;
phones, empowers users to effortlessly select specific location points, streamlining navi&#xD;
gation within intricate indoor spaces. A key highlight of the system is its utilization of &#xD;
LED lights; each assigned a unique color, to guide users along the optimal path leading &#xD;
to different destinations. This innovative approach provides clear visual cues enhancing &#xD;
user orientation. Moreover, when transitioning to different indoor locations, the system &#xD;
seamlessly incorporates a map display feature through the app, offering users a compre&#xD;
hensive view of their surroundings. The microcontroller-based control system ensures the &#xD;
synchronization of LED lights and map displays, offering users a user-friendly and effi&#xD;
cient means of navigating complex environments. Bluetooth modules facilitate real-time &#xD;
communication between the app and the system, ensuring timely updates and responsive &#xD;
interaction. This research contributes to the advancement of self-navigation systems, par&#xD;
ticularly in multi-story buildings where traditional navigation solutions may fall short. &#xD;
The seamless integration of microcontroller technology, LED lights, and Bluetooth mod&#xD;
ules establishes a robust platform for creating an intelligent and accessible self&#xD;
navigation experience. The proposed system not only streamlines navigation within di&#xD;
verse indoor environments but also enhances user interaction through an intuitive app in&#xD;
terface, thus addressing the evolving needs of modern navigational systems.</summary>
    <dc:date>2024-01-01T00:00:00Z</dc:date>
  </entry>
  <entry>
    <title>Process enhancement and performance evaluation of single‑shot  drilling of CFRP/aluminum stacks: a review</title>
    <link rel="alternate" href="http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/11807" />
    <author>
      <name>Joy Mathavan, J.</name>
    </author>
    <author>
      <name>Hassan, Muhammad Hafiz</name>
    </author>
    <id>http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/11807</id>
    <updated>2025-11-24T09:00:53Z</updated>
    <published>2025-01-01T00:00:00Z</published>
    <summary type="text">Title: Process enhancement and performance evaluation of single‑shot  drilling of CFRP/aluminum stacks: a review
Authors: Joy Mathavan, J.; Hassan, Muhammad Hafiz
Abstract: Drilling is an essential process in the construction of aircraft panels made from composite/metal stack materials, and it has &#xD;
a considerable impact on the performance of the aircraft during flight and its overall lifespan. Among CFRP/Al/Ti, CFRP/&#xD;
 Ti, and CFRP/Al stacks, CFRP/Al panels are widely used in the aviation industry. This paper examines in detail the develop&#xD;
ments made in the drilling of stacks made of carbon fiber reinforced polymer (CFRP) and aluminum (Al), with the goal of &#xD;
determining how different machining parameters affect the quality of the holes. The primary requirements for aircraft com&#xD;
ponents are to attain a low level of hole surface roughness, minimize burr heights, reduce the diameter difference in stack-up, &#xD;
and minimize delamination. The subject matter encompasses a wide range of tool shapes, materials, drilling parameters, and &#xD;
innovative methods of cooling and coating, all with the goal of reducing hole damage and improving quality. In addition, the &#xD;
paper examines several forms of hole damage and presents modern methodologies for their quantification. This review study &#xD;
aims to develop a reliable standard for achieving accuracy, optimal productivity, and reducing harm in the drilling procedure &#xD;
of CFRP/Al stacks in aerospace applications. Future works on analysis of bond strength, hardness, and coefficient of friction &#xD;
of coated drill bits and application of nano fluid-based coolants may further enhance the drilling quality</summary>
    <dc:date>2025-01-01T00:00:00Z</dc:date>
  </entry>
  <entry>
    <title>Comprehensive review of drilling strategies for CFRP/Ti  s  tacks in aircraft manufacturing</title>
    <link rel="alternate" href="http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/11806" />
    <author>
      <name>Joy Mathavan, J.</name>
    </author>
    <author>
      <name>Hassan, M.H.</name>
    </author>
    <id>http://repo.lib.jfn.ac.lk/ujrr/handle/123456789/11806</id>
    <updated>2025-11-24T08:58:54Z</updated>
    <published>2025-01-01T00:00:00Z</published>
    <summary type="text">Title: Comprehensive review of drilling strategies for CFRP/Ti  s  tacks in aircraft manufacturing
Authors: Joy Mathavan, J.; Hassan, M.H.
Abstract: Single-shot drilling of carbon fiber-reinforced polymer/titanium &#xD;
alloy stacks in aerospace applications poses unique challenges. &#xD;
The interaction between the cutting tool and the composite- &#xD;
metal contact often leads to poor hole quality and increased &#xD;
tool wear. The review extensively examines research achieve&#xD;
ments and developments in drilling CFRP/Ti stacks to compre&#xD;
hensively assess the impact of various machining settings on &#xD;
hole quality. Contributing factors such as stack-up machining &#xD;
thrust force, temperature, chip form and tool wear characteris&#xD;
tics are thoroughly investigated. Moreover, this article high&#xD;
lights manufacturing defects in metallic and composite panels &#xD;
during drilling operations, contributing to a higher rejection &#xD;
rate in the assembly process. Usually, the maximum delamin&#xD;
ation of 1mm, diameter deviation of ±30mm, burr height of &#xD;
150mm, metal part’s surface roughness of 1.6mm and CFRP &#xD;
part’s surface roughness of 3.2mm are allowed in the aero&#xD;
space industry. Additionally, the research explores strategies &#xD;
to mitigate manufacturing defects, including measures to limit &#xD;
hole and tool damage. These tactics encompass tool structure, &#xD;
machining environment, machining parameters and machin&#xD;
ing technology. On the whole, this review study aims to fill &#xD;
the research gap regarding process enhancement and per&#xD;
formance evaluation of single-shot drilling of CFRP/Ti stacks in &#xD;
aerospace applications.</summary>
    <dc:date>2025-01-01T00:00:00Z</dc:date>
  </entry>
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