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Questions related from Noorul Huda
I have a lab combustor on which I did some experiments and obtained some flashback data in terms of equivalence ratio at various flow conditions. i want to simulate the reacting flow field at...
13 June 2021 6,999 1 View
I want to calculate the equivalence ratio for a fuel air mixture containing two fuels methane and hydrogen and the oxidizer is air. I am calculating equivalence ratio as, phi=[(wt. CH4+wt....
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I am studying the near blowout instability mechanism in gas turbine combustors where I often come different pressure sensors. Some are dynamic pressure transducers while others are microphones....
10 January 2021 8,440 3 View
We have an optically accessible atmospheric combustor. We want to perform the instability analysis of the combustor like flashback, blowout and instabilities occurring near lean blowout. We are...
26 October 2020 2,478 1 View
I am designing a Lean Premixed swirl stabilized Combustor which has a premixer tube where fuel and air are mixed prior to combustion in the combustion chamber. What is the typical maximum flow...
13 October 2020 7,566 5 View
I am designing a gas turbine combustor test rig for my research activities. To ensure a uniform distribution of air going into the combustion chamber, I would like to attach a plenum/settling...
04 September 2020 2,832 4 View
I am working on a design of Lean Premixed combustor. The combustion chamber is of can type with varying liner cross section area similar to the one shown in the attached figure. My question is how...
13 May 2020 4,512 0 View
The mixing of two fluids is due to advection only. There is no heat transfer involved. The two working fluids are dye and water in a simple T-microchannel
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