<?xml version="1.0" encoding="UTF-8"?>
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  <title>DSpace Community:</title>
  <link rel="alternate" href="http://210.212.227.212:8080/xmlui/handle/123456789/142" />
  <subtitle />
  <id>http://210.212.227.212:8080/xmlui/handle/123456789/142</id>
  <updated>2026-05-27T20:52:59Z</updated>
  <dc:date>2026-05-27T20:52:59Z</dc:date>
  <entry>
    <title>INVESTIGATION ON THE CAPACITANCE FLOWMETER &amp; DEVELOPMENT OF VOID FRACTION SENSOR FOR CRYOGENIC TWO-PHASE FLOW</title>
    <link rel="alternate" href="http://210.212.227.212:8080/xmlui/handle/123456789/599" />
    <author>
      <name>Archana, Mohan</name>
    </author>
    <author>
      <name>Mathew, Skaria</name>
    </author>
    <id>http://210.212.227.212:8080/xmlui/handle/123456789/599</id>
    <updated>2024-07-15T09:20:38Z</updated>
    <published>2024-06-03T00:00:00Z</published>
    <summary type="text">Title: INVESTIGATION ON THE CAPACITANCE FLOWMETER &amp; DEVELOPMENT OF VOID FRACTION SENSOR FOR CRYOGENIC TWO-PHASE FLOW
Authors: Archana, Mohan; Mathew, Skaria
Abstract: Cryocoolers are devices that produce very low temperatures and provide adequate amount of&#xD;
cooling power at a specific location and hence can replace the conventional cryogenic fluids.&#xD;
The main difference between cryocoolers and cryogenic fluids is that cryocoolers can produce&#xD;
refrigeration at various low temperatures, while cryogenic fluids only provide refrigeration at&#xD;
specific temperatures, namely their boiling points.&#xD;
Cryocoolers can be classified into different types based on the heat exchangers used in them.&#xD;
They are regenerative and recuperative types. Regenerative type cryocoolers are further&#xD;
classified into three types namely, Stirling, Gifford McMahon (GM) and Pulse Tube.&#xD;
The CTI GM type cryocooler (Model: Cryodyne, Number:350C) had been chosen in our&#xD;
studies to understand its design, working and also to reverse engineer its development. One&#xD;
could learn the assembly of the system and also how it can be dismantled without damaging&#xD;
the components. After preparing the dimensional drawing of the displacer, Bakelite has been&#xD;
used for its fabrication, since it forms an equivalent substitute for the original Micarta material.&#xD;
The newly fabricated displacer housing was filled with the original regenerator materials and&#xD;
assembled into the coldhead housing. The temperature sensors were incorporated for the first&#xD;
and second stage cold heads. The system was tested for its performance to determine its lowest&#xD;
temperature reached.&#xD;
The regenerator materials and the sealings form the crucial components for the improved&#xD;
performance of the cryocooler. Both Teflon split rings and Rulon split rings have been used as&#xD;
sealings in our studies. Presently second stage temperature ~11.5K has been measured with&#xD;
lead as the regenerator material, with a water cooled 3kW helium compressor. On the other&#xD;
hand, with 1.5kW helium compressor, a temperature of 14.7K has been measured with lead as&#xD;
the regenerator material. With the same helium compressor, temperatures of 15.48K and&#xD;
19.45K have been measured with Holmium copper and Erbium Nickel as regenerator materialrespectively. Since the above values are higher than those of with Lead as regenerator, we&#xD;
suspect the above regenerator materials have aged and are not performing satisfactorily.&#xD;
The first stage temperatures have been measured as 75.96 K and 58.93 K for Holmium copper&#xD;
and Erbium Nickel as second stage regenerator materials respectively. The first stage&#xD;
regenerator material used in the setup is copper meshes (&lt; 200 mesh size).&#xD;
We have successfully designed and fabricated the displacer housing of the GM cryocooler&#xD;
system. Experiment have been performed using both labyrinth and non-labyrinth type housing.&#xD;
The performance of the system with indigenously designed displacer is quite satisfactory.&#xD;
Also, the theoretical analysis of the single stage GM Cryocooler has been attempted using the&#xD;
open-source regions software. By this analysis one can evaluate the cooling power, COP and&#xD;
inefficiency of the system as a function of various design and operational parameters.&#xD;
Following are the outcomes of the project.&#xD;
1. Complete design drawings of the first and second stage displacer along with its housing.&#xD;
2. Both Labyrinth type and non-labyrinth type displacers I have been designed, fabricated and&#xD;
tested.&#xD;
3. Teflon silly rings are formed to perform better than the plastic sealing rings&#xD;
The results indicate that the performance of the regenerator materials such as Holmium Copper&#xD;
and Erbium Nickel is not satisfactory due to the aging effect and perhaps one should look for&#xD;
fresh regenerator materials.</summary>
    <dc:date>2024-06-03T00:00:00Z</dc:date>
  </entry>
  <entry>
    <title>DEVELOPMENT OF TWO STAGE GIFFORD McMAHON CRYOCOOLER</title>
    <link rel="alternate" href="http://210.212.227.212:8080/xmlui/handle/123456789/598" />
    <author>
      <name>Rahul, R</name>
    </author>
    <author>
      <name>Rijo Jacob, Thomas</name>
    </author>
    <id>http://210.212.227.212:8080/xmlui/handle/123456789/598</id>
    <updated>2024-07-15T09:15:09Z</updated>
    <published>2024-06-03T00:00:00Z</published>
    <summary type="text">Title: DEVELOPMENT OF TWO STAGE GIFFORD McMAHON CRYOCOOLER
Authors: Rahul, R; Rijo Jacob, Thomas
Abstract: Cryogenic fluids have significant growth in different industrial applications, including superconductivity,&#xD;
aerospace etc. Depending on the application, the cryogenic fluid flow's purpose varies greatly. Cryogens&#xD;
are required in the case of superconducting magnets in order to maintain the magnet material below a&#xD;
certain temperature and preserve the superconducting state. Currently, no one technology is capable of&#xD;
measuring two-phase flow throughout the entire range of flow conditions. Presenting the design and testing&#xD;
of the proposed two-phase flow-metering device is the goal. The concept is to use capacitance to measure&#xD;
the liquid's height at various locations in the channel by forcing the flow into both a laminar and stratified&#xD;
flow regime. In theory, the flow-rate can be inferred from these height measurements. The idea is a two-&#xD;
phase flow of vapor and liquid through small, parallel channels that produces a laminar, stratified flow that&#xD;
slopes at the liquid-vapor interface. Capacitance-liquid level devices are used in the channel to measure&#xD;
the liquid height. G10 printed circuit boards (PCBs) are used to create the channel walls, and the capacitor&#xD;
conductors are electroplated directly onto the boards to minimize channel intrusion.</summary>
    <dc:date>2024-06-03T00:00:00Z</dc:date>
  </entry>
  <entry>
    <title>NUMERICAL INVESTIGATIONS ON SYNTHETIC JET  IMPINGEMENT COOLING USING MULTIPLE ORIFICE</title>
    <link rel="alternate" href="http://210.212.227.212:8080/xmlui/handle/123456789/466" />
    <author>
      <name>Vaishnav, S</name>
    </author>
    <author>
      <name>Shafi, K A</name>
    </author>
    <id>http://210.212.227.212:8080/xmlui/handle/123456789/466</id>
    <updated>2023-10-07T07:13:57Z</updated>
    <published>2023-05-01T00:00:00Z</published>
    <summary type="text">Title: NUMERICAL INVESTIGATIONS ON SYNTHETIC JET  IMPINGEMENT COOLING USING MULTIPLE ORIFICE
Authors: Vaishnav, S; Shafi, K A
Abstract: A synthetic jet generally consists of a cavity with a driver attached on one side and an orifice on &#xD;
the opposite side. When the driver moves back and forth, the jet will generate an unsteady flow &#xD;
through the orifice and the flow will move downstream to a surface forming an impinging flow. &#xD;
When the jet is in the ejection cycle, the diaphragm will expel flow out from the orifice and form &#xD;
a vortex near the orifice. If the propulsion is large enough, the vortex will move downstream &#xD;
before the jet orifice flow reverses and starts to suck in flow. The computational process is &#xD;
carried out using the commercial software ANSYS Fluent. In this study, the heat transfer &#xD;
characteristics of synthetic jet impingement cooling with multiple orifice (2,4 and 16 orifices) &#xD;
are analyse with different operating frequencies (f=1Hz to f=5Hz and f=100Hz to f=500Hz) with &#xD;
different Reynolds number (Re=5000,10000 and 20000) well as Strouhal number (St=0.006 to &#xD;
St=0.030). The results demonstrate that high frequency synthetic jets show better heat removal &#xD;
capacity than lower frequency at the same Reynolds number. Also, the variation of area averaged Nusselt number depends on Strouhal number or dimensionless stroke length.</summary>
    <dc:date>2023-05-01T00:00:00Z</dc:date>
  </entry>
  <entry>
    <title>EFFECT OF CRYOGENIC TREATMENT ON  THERMAL AND MECHANICAL PROPERTIES OF  HEMP FIBER COMPOSITE PANELS</title>
    <link rel="alternate" href="http://210.212.227.212:8080/xmlui/handle/123456789/465" />
    <author>
      <name>Rahul, Raj</name>
    </author>
    <author>
      <name>Shafi, K A</name>
    </author>
    <id>http://210.212.227.212:8080/xmlui/handle/123456789/465</id>
    <updated>2023-10-07T07:08:04Z</updated>
    <published>2023-05-01T00:00:00Z</published>
    <summary type="text">Title: EFFECT OF CRYOGENIC TREATMENT ON  THERMAL AND MECHANICAL PROPERTIES OF  HEMP FIBER COMPOSITE PANELS
Authors: Rahul, Raj; Shafi, K A
Abstract: Natural fibres have been outstanding materials which are feasible and amble substitute for &#xD;
expensive, non-bio degradable and non-renewable synthetic materials so these organic/natural &#xD;
fibres can be used as replacement for synthetic fibers for various applications. Cryogenic &#xD;
treatment is a type of heat treatment process applied to materials at low temperatures in which &#xD;
fiber is treated at cryogenic temperatures, at this low temperature conditions, materials showcase &#xD;
some physiochemical changes The main objective of these works is to conduct cryogenic &#xD;
treatment on hemp fiber and to study the effect of cryogenic treatment on thermal, mechanical &#xD;
and water absorption properties of hemp fiber reinforced epoxy composite panels. Physical &#xD;
properties such as functional groups of fabrics were studied and compared using Fourier &#xD;
Transform Infrared Spectroscopy (FTIR). It shows treatment on fiber have substantially &#xD;
increased the number of hydrogen bonding in cellulose, which lead to increase in stiffness of the &#xD;
fabric. The thermal behaviour of untreated and treated hemp fiber was studied using the &#xD;
techniques of thermo gravimetric analysis (TGA) and differential thermo gravimetric analysis &#xD;
(DTG). It is observed that after cryogenic treatment, hemp fiber's thermal stability has been &#xD;
significantly enhanced. Mechanical properties such as tensile and flexural strength of &#xD;
Hemp/epoxy panels are studied under untreated and cryogenic treated condition and the result &#xD;
show improvement in mechanical properties under cryogenic treatment. Improvement in &#xD;
mechanical properties was observed in cryogenic treated hemp composite due to increased &#xD;
frictional bond in the composite interface. Thermal conductivity of panels was measured using &#xD;
guarded hot plate method and the results shows decrease in thermal conductivity after cryogenic &#xD;
treatment. Water absorption rate of the fiber increases with time due to hygroscopic nature of &#xD;
fiber.Cryogenic treated hemp fiber shows 12% reduction in percentage of water absorption &#xD;
compared to untreated hemp fiber. These findings indicate hemp fabric as an alternative bio degradable material with greater thermal stability and physical qualities than synthetic materials &#xD;
for engineering applications</summary>
    <dc:date>2023-05-01T00:00:00Z</dc:date>
  </entry>
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