PRELIMINARY DESIGN AND NUMERICAL SIMULATION OF A REVERSE FLOW ANNULAR COMBUSTOR AT BASIC DESIGN POINT OPERATING CONDITIONS

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@article{1700761,
      author = {DEEPA M S, Dr. A AROKKIASWAMY},
      title = {PRELIMINARY DESIGN AND NUMERICAL SIMULATION OF A REVERSE FLOW ANNULAR COMBUSTOR AT BASIC DESIGN POINT OPERATING CONDITIONS},
      journal = {Iconic Research And Engineering Journals},
      year = {2018},
      volume = {2},
      number = {4},
      pages = {17-22},
      issn = {2456-8880},
      url = {https://www.irejournals.com/formatedpaper/1700761.pdf},
      abstract = {This paper presents the preliminary design methodology for a Reverse flow annular combustor based on calculation of the geometric parameters, gas temperature profile, liner wall temperatures and position of air admission holes for a small gas turbine engine with Jet A as fuel. It also includes the modelling and numerical simulation of temperature distribution at centerline, inlet and outlet of the combustor using Ansys-CFX, carried out at basic design point operating conditions.},
      keywords = {Reverse flow annular combustor, numerical simulation, Ansys-CFX, operating conditions},
      month = {October},
  }