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    <title>DSpace Collection:</title>
    <link>http://dspace.dtu.ac.in:8080/jspui/handle/123456789/220</link>
    <description />
    <items>
      <rdf:Seq>
        <rdf:li rdf:resource="http://dspace.dtu.ac.in:8080/jspui/handle/repository/20193" />
        <rdf:li rdf:resource="http://dspace.dtu.ac.in:8080/jspui/handle/repository/19750" />
        <rdf:li rdf:resource="http://dspace.dtu.ac.in:8080/jspui/handle/repository/19735" />
        <rdf:li rdf:resource="http://dspace.dtu.ac.in:8080/jspui/handle/repository/19627" />
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    </items>
    <dc:date>2026-04-28T04:03:35Z</dc:date>
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  <item rdf:about="http://dspace.dtu.ac.in:8080/jspui/handle/repository/20193">
    <title>STUDY OF GAS TURBINE COGENERATION CYCLE  WITH INLET EVAPORATIVE COOLING AND  REHEATING</title>
    <link>http://dspace.dtu.ac.in:8080/jspui/handle/repository/20193</link>
    <description>Title: STUDY OF GAS TURBINE COGENERATION CYCLE  WITH INLET EVAPORATIVE COOLING AND  REHEATING
Authors: RAUTELA, JYOTI
Abstract: Energy has been a major concern over the years all over the world. Cogeneration is being coined &#xD;
as the efficient utilization of energy in various power plants. Gas turbine being the compact and &#xD;
one of the most reliable means for the generation of power is pretty good to be used for &#xD;
cogeneration. Cogeneration in general is a term used for producing heat and work &#xD;
simultaneously. The exhaust heat from the turbine is used as the process steam for either district &#xD;
heating, cooling at various applications. Cogeneration with gas turbines is the frequently and &#xD;
widely used cogeneration system because this type of system takes the advantage of the relative &#xD;
merit of engine and enhances thermal efficiency at full load conditions as well as part load &#xD;
conditions. Also, it is highly accepted in power industries.&#xD;
The work performed provides a review of research investigation on cogeneration systems &#xD;
which are carried out during the last few years. Along with the literature review, the &#xD;
performance of various output parameters of gas turbine cogeneration system with reheat and &#xD;
inlet evaporative cooling (proposed cycle) are analyzed parametrically taking compressor &#xD;
pressure ratio, turbine inlet temperature, pinch point temperature and inlet temperature of air as &#xD;
the main variables. The effect of these parameters on power/specific work, efficiency, power to &#xD;
heat ratio, First law efficiency and second law efficiency were plotted with the help of EES &#xD;
software.</description>
    <dc:date>2020-08-01T00:00:00Z</dc:date>
  </item>
  <item rdf:about="http://dspace.dtu.ac.in:8080/jspui/handle/repository/19750">
    <title>COMPARATIVE ENERGY AND EXERRGY ANALYSIS OF ORC-VCR  AND MODIFIED ORC-VCR CYCLE USING DIFFERENT WORKING  FLUIDS</title>
    <link>http://dspace.dtu.ac.in:8080/jspui/handle/repository/19750</link>
    <description>Title: COMPARATIVE ENERGY AND EXERRGY ANALYSIS OF ORC-VCR  AND MODIFIED ORC-VCR CYCLE USING DIFFERENT WORKING  FLUIDS
Authors: SUKHDAVE, AKITA
Abstract: This study examines the energy and exergy of a solar-powered Organic Rankine Cycle &#xD;
(ORC) that uses the refrigerants R245fa, R602, and R600 as working fluid to generate &#xD;
electricity. The suggested cycle combines a solar-sub system with a heliostat and a &#xD;
central receiver with an ORC. The rate of exergy destruction (irreversibility) in each &#xD;
component of the ORC cycle is calculated to assess the cycle's actual performance as &#xD;
well as the causes and locations of thermodynamic imperfection.&#xD;
Using the first and second law technique, parametrical analysis is used to determine the &#xD;
influence of different operational factors on the performance of the ORC Cycle. The &#xD;
impact of several operating factors including turbine input pressure, turbine back &#xD;
pressure, and condenser temperature on energy and exergy efficiency, as well as &#xD;
irreversibility in ORC components such the heat recovery vapour generator, turbine, &#xD;
condenser, and pump, was investigated. Energy efficiency rises from 9.74 percent to &#xD;
11.3 percent and exergetic efficiency increases from 10.43 percent to 12.10 percent &#xD;
with an increase in turbine intake pressure (1.58-2.38 MPa). The energy and exergy &#xD;
efficiency drops from 11.62 percent to 9.80 percent and 12.44 percent to 10.44 percent &#xD;
with an increase in turbine back pressure (0.18-0.26 MPa). Using R600, R602, and &#xD;
R245fa, the suggested solar-powered ORC cycle will be beneficial for power &#xD;
generation.</description>
    <dc:date>2021-08-01T00:00:00Z</dc:date>
  </item>
  <item rdf:about="http://dspace.dtu.ac.in:8080/jspui/handle/repository/19735">
    <title>NUMERICAL SIMULATION OF SINGLE AND DOUBLE  SLOPE SOLAR STILL FOR DIFFERENT VARIABLES</title>
    <link>http://dspace.dtu.ac.in:8080/jspui/handle/repository/19735</link>
    <description>Title: NUMERICAL SIMULATION OF SINGLE AND DOUBLE  SLOPE SOLAR STILL FOR DIFFERENT VARIABLES
Authors: KUMAR, ROHIT
Abstract: Water and the use of conventional energy sources are two significant problems in the &#xD;
world. Water is essential for sustenance. Human beings need of potable water at less &#xD;
consumption of non- renewable energy resources. There are many techniques to convert &#xD;
saline water into potable water. In this paper, three-phase, three dimensional a single slope &#xD;
and double slope single basin still both were prepared and simulated by using ANSYS &#xD;
FLUENT v19.2. Simulation results of solar stills were made by using evaporation as well &#xD;
as condensation process at the climate conditions of Delhi (27.0238° N, 74.2179° E). &#xD;
Within the scope of this study, simulation results of both systems were calculated and &#xD;
compared with each other. It is examined that the temperature inside the single slope solar &#xD;
still is maximum from 13:00 to 14:00 hrs while the double slope still has low temperature &#xD;
compared to the single still. The maximum and minimum temperature of the water-vapor &#xD;
mixture inside the single slope still were calculated 435.39K and 22.283K and the &#xD;
maximum and minimum temperature on glass were 379 K and 16.22 K whereas in double &#xD;
slope, the maximum and minimum temperature of the water-vapor mixture inside the still &#xD;
were 92.12K and 25.60K and glass temperature were 76.154K and 19.22K. Hence, due to &#xD;
the temperature difference between the glass surface and outer environment, more &#xD;
condensation will be in the single slope solar still. Inner water temperature is responsible &#xD;
for more evaporation and higher temperature more than 50℃ can be found in single slope &#xD;
solar still as compared to the double slope. The maximum water production rate in single &#xD;
slope solar still is 0.84 kg m-2&#xD;
hr-1 while the maximum water production rate in the double &#xD;
slope is 0.26 kg m-2&#xD;
hr-1&#xD;
. In the simulation, all other variables are also checked and &#xD;
calculated, also observed single slope solar still has a high value of all variables which &#xD;
affect water production. Hence, the single slope solar still could be better there.</description>
    <dc:date>2020-08-01T00:00:00Z</dc:date>
  </item>
  <item rdf:about="http://dspace.dtu.ac.in:8080/jspui/handle/repository/19627">
    <title>SOME STUDIES ON ENGINE COMBUSTION, EMISSION, AND  SPRAY CHARACTERISTICS OF A CRDI DIESEL ENGINE  WITH VARIABLE NOZZLE GEOMETRY USING ANSYS</title>
    <link>http://dspace.dtu.ac.in:8080/jspui/handle/repository/19627</link>
    <description>Title: SOME STUDIES ON ENGINE COMBUSTION, EMISSION, AND  SPRAY CHARACTERISTICS OF A CRDI DIESEL ENGINE  WITH VARIABLE NOZZLE GEOMETRY USING ANSYS
Authors: SINGH, VAIBHAV SINGH
Abstract: The present study aims to investigate the effect on combustion, emission, &#xD;
and spray characteristics with the variation of the nozzle hole diameters &#xD;
(NHD) in a diesel engine. For this a CFD 3D model is developed for a four stroke diesel engine fueled with neat diesel and three different NHD, i.e., &#xD;
0.20 mm, 0.26 mm, and, 0.30 mm. The CFD 3D models were effectively &#xD;
able to predict the turbulence and turbulent-flame propagation interaction, &#xD;
chemistry involved in combustion processes, and the dissociation and &#xD;
reassociation of chemical species. For the model validation, the &#xD;
combustion characteristics of the CRDI-VCR engine are used. The &#xD;
validation results showed good compatibility having the relative error &#xD;
within the range. The analysis showed that increasing the nozzle hole &#xD;
diameter resulted in the decrease of the in-cylinder pressure by about &#xD;
8.31% and 31.93%, respectively, for 0.26 mm and 0.30 mm diameter &#xD;
compared to 0.20 mm. The AHRR also showed a similar trend with a &#xD;
decrease of about 11.82% and 42.18%, respectively, for 0.26 mm and 0.30 &#xD;
mm diameter as compared to 0.20 mm. Subsequently, the increase in &#xD;
nozzle diameter showed an increase in HC and CO emissions but a &#xD;
decrease in NOx emissions. The CO emissions increase by about 0.65% &#xD;
and 5.08% and HC emissions increase by about 29.90% and 60.13% &#xD;
respectively for 0.26 mm and 0.30 mm diameter compared to 0.20 mm. &#xD;
viii&#xD;
While the NOx emission reduces by about 41.18% and 70.58% &#xD;
respectively for 0.26 mm and 0.30 mm diameter as compared to 0.20 mm. &#xD;
The effect of different nozzle diameters on spray characteristics is analyzed &#xD;
and verified from previous studies. The increase in nozzle diameter showed &#xD;
an increase in liquid penetration length, breakup length, and SMD. Also, &#xD;
the present study shows the possibilities of the CFD models for the &#xD;
simulation of engines employing different fuels and operative conditions.</description>
    <dc:date>2021-10-01T00:00:00Z</dc:date>
  </item>
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