Dergi makalesi Açık Erişim

Effects of turbulence and flamelet combustion modelling on the CFD simulation of a dual inlet ramjet combustor

Solmaz, Mehmet Burak; Uslu, Sitki


MARC21 XML

<?xml version='1.0' encoding='UTF-8'?>
<record xmlns="http://www.loc.gov/MARC21/slim">
  <leader>00000nam##2200000uu#4500</leader>
  <datafield tag="260" ind1=" " ind2=" ">
    <subfield code="c">2023-01-01</subfield>
  </datafield>
  <datafield tag="100" ind1=" " ind2=" ">
    <subfield code="a">Solmaz, Mehmet Burak</subfield>
  </datafield>
  <datafield tag="540" ind1=" " ind2=" ">
    <subfield code="u">http://www.opendefinition.org/licenses/cc-by</subfield>
    <subfield code="a">Creative Commons Attribution</subfield>
  </datafield>
  <datafield tag="700" ind1=" " ind2=" ">
    <subfield code="u">TOBB Univ Econ &amp; Technol, TR-06560 Ankara, Turkiye</subfield>
    <subfield code="a">Uslu, Sitki</subfield>
  </datafield>
  <datafield tag="909" ind1="C" ind2="O">
    <subfield code="o">oai:aperta.ulakbim.gov.tr:265588</subfield>
    <subfield code="p">user-tubitak-adresli-yayinlar</subfield>
  </datafield>
  <datafield tag="542" ind1=" " ind2=" ">
    <subfield code="l">open</subfield>
  </datafield>
  <datafield tag="520" ind1=" " ind2=" ">
    <subfield code="a">&lt;p&gt;This manuscript presents Computational Fluid Dynamics simulation of a ramjet combustor using Reynolds Averaged Navier-Stokes approach for turbulence with flamelet combustion modelling. In the approach a one-dimensional premixed flame simulation is performed to cover a wide range of mixture fraction space. After a mesh study, effects of turbulence, Realizable k-e and SST k-?, and combustion modelling, Steady Laminar Flamelet and Flamelet Generated Manifold, are investigated in detail. The Flamelet Generated Manifold model that offers a reaction delay by employing an additional progress variable, shows there are no reactions taking place in the vicinity of jet inlets, hence the unrealistic temperature rise that is seen in the case of using Steady Laminar Flamelet is not observed. A study on the choice of progress variable based on the combustion products is carried out. The present study readily demonstrates good predictability of Flamelet Generated Manifold combustion modelling in such a dual inlet ramjet combustion chamber.&lt;/p&gt;</subfield>
  </datafield>
  <datafield tag="024" ind1=" " ind2=" ">
    <subfield code="a">10.1515/tjj-2023-0039</subfield>
    <subfield code="2">doi</subfield>
  </datafield>
  <controlfield tag="005">20240607113802.0</controlfield>
  <datafield tag="245" ind1=" " ind2=" ">
    <subfield code="a">Effects of turbulence and flamelet combustion modelling on the CFD simulation of a dual inlet ramjet combustor</subfield>
  </datafield>
  <datafield tag="909" ind1="C" ind2="4">
    <subfield code="c">9</subfield>
    <subfield code="p">INTERNATIONAL JOURNAL OF TURBO &amp; JET-ENGINES</subfield>
  </datafield>
  <datafield tag="650" ind1="1" ind2="7">
    <subfield code="2">opendefinition.org</subfield>
    <subfield code="a">cc-by</subfield>
  </datafield>
  <controlfield tag="001">265588</controlfield>
  <datafield tag="980" ind1=" " ind2=" ">
    <subfield code="a">user-tubitak-adresli-yayinlar</subfield>
  </datafield>
  <datafield tag="980" ind1=" " ind2=" ">
    <subfield code="b">article</subfield>
    <subfield code="a">publication</subfield>
  </datafield>
  <datafield tag="856" ind1="4" ind2=" ">
    <subfield code="u">https://aperta.ulakbim.gov.trrecord/265588/files/bib-3b4ae8dd-ff48-45e5-b85d-9d38f85714f4.txt</subfield>
    <subfield code="z">md5:e1667963090a098528578563cc9da762</subfield>
    <subfield code="s">194</subfield>
  </datafield>
</record>
35
6
görüntülenme
indirilme
Görüntülenme 35
İndirme 6
Veri hacmi 1.2 kB
Tekil görüntülenme 32
Tekil indirme 6

Alıntı yap