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The output from the model includes the apparent heat release, fraction of fuel burned, fuel burning rate, heat losses, indicated parameters and average gas temperature.
The zero-dimensional model is based on the first law of thermodynamics in which an empirical relationship between the fuel burning rate and crank angle position is established.
Steady-state theory correlates the end-of-drop experimental data, including the theoretical flame shape and fuel burning rate.
As pressure increases, the fuel burning rate decreases slightly and then increases considerably, which is attributed to the effect of pressure on heat transfers.
The simulation model includes detailed sub-models for fuel burning rate, combustion products, thermodynamic properties of working fluid, heat transfer, fluid flow, and both soot and oxides of nitrogen (NOx) formation mechanisms.
Different fuels, chemical mechanisms, and equivalence ratios are considered and their effects on turbulent flame speed, geometry of the reaction zone, and fuel burning rate are analyzed.
Similar(46)
The flow rate of methane is 0.066 kg/m2-s, comparable to fuel burning rates in a large JP8 pool fire.
In the unity Lewis number limit, the n-heptane, iso-octane, toluene, and methane flames at a given reaction zone Karlovitz number present similar normalized turbulent flame speeds and fuel burning rates close to their respective laminar values.
A new concept of reverse fuel injection is introduced to enhance the fuel-burning rate in upward swirl can-type gas turbine combustor.
In fact, the flame length is directly related to the fuel evaporation rate essentially, hence, the cross wind and fuel spacing will affect the flame length by changing fuel evaporation and burning rate.
The difference of combustion characteristics under different pressure environment were investigated, combustion characteristics of ethanol pool fire, such as fuel's mass burning rate, flame shape, flame centre-line temperature and plume velocity in different ambient pressure conditions were measured.
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