Now showing items 1-4 of 4

    • Aerodynamic study of combustor using axial swirler 

      Mohammad Nazri, Jaafar; M. K. F., M. Nor; Mohamad Shaiful Ashrul, Ishak (Praise Worthy Prize S.r.l., 2011-01)
      A study has been conducted to investigate the flow pattern in a gas turbine combustion chamber by simulation and experimental approaches. Flow pattern inside a combustor is important to self sustain the flame, increase ...
    • Combustor aerodynamic using radial swirler 

      Mohammad Nazri, Mohd Jaafar, Prof. Dr.; Jusoff, Kamarudin, Prof. Dr.; Mohamed Seroleh, Osman; Mohd Shaiful Ashrul, Ishak (Academic Journals, 2011-07)
      A study has been conducted to investigate the flow pattern in a gas turbine combustion chamber by simulation and experimental approaches. Flow pattern inside a combustor is important to self sustain the flame, increase ...
    • The effect of radial swirl generator on reducing emissions from bio-fuel burner system 

      Mohamad Shaiful Ashrul, Ishak; Mohammad Nazri, Mohd Jaafar; A. Eldrainy, Yehia (Canadian Center of Science and Education, 2009-06)
      A liquid bio-fuel burner system with various radial air swirlers attached to combustion chamber of 280 mm inside diameter and 1000 mm length has been investigated. All tests were conducted using crude palm oil as fuel. A ...
    • Effect of velocity variation at high swirl on axial flow development inside a can combustor 

      Mohamad Shaiful, Ashrul Ishak; Mohammad Nazri, Mohd Jaafar, Prof. Dr. (Penerbit UTM Press, 2014)
      The main purpose of this paper is to study the internal flow effect of varying the inlet velocities inside a combustor. The flow field inside the combustor is controlled by the liner shape and size, wall side holes shape, ...