Low-temperature zone of the front of hydrocarbon flames VI. Oxidation of hexane near flame front

1978 ◽  
Vol 13 (4) ◽  
pp. 547-549
Author(s):  
G. I. Ksandopulo ◽  
B. Ya. Kolesnikov ◽  
V. V. Dubinin ◽  
D. S. Odnorog
1975 ◽  
Vol 11 (6) ◽  
pp. 714-719
Author(s):  
G. I. Ksandopulo ◽  
A. A. Sagindykov ◽  
S. E. Kudaibergenov ◽  
Z. A. Mansurov

1976 ◽  
Vol 11 (1) ◽  
pp. 52-57
Author(s):  
G. I. Ksandopulo ◽  
B. Ya. Kolesnikov ◽  
D. S. Odnorog

1976 ◽  
Vol 11 (1) ◽  
pp. 114-117
Author(s):  
G. I. Ksandopulo ◽  
B. Ya. Kolesnikov ◽  
D. S. Odnorog

1982 ◽  
Vol 18 (6) ◽  
pp. 637-639
Author(s):  
V. K. Manzhos ◽  
B. Ya. Kolesnikov ◽  
A. K. Murzagaliev ◽  
G. I. Ksandopulo

1976 ◽  
Vol 11 (3) ◽  
pp. 350-354
Author(s):  
G. I. Ksandopulo ◽  
B. Ya. Kolesnikov ◽  
D. S. Odnorog ◽  
V. V. Dubinin

2021 ◽  
pp. 83-90
Author(s):  
Alyona Shilova ◽  
◽  
Nikolay Bachev ◽  
Roman Bulbovich ◽  
◽  
...  

For a stable position of the flame front in the combustion chambers of gas turbine power plants, the fresh gas-air mixture must be heated to the ignition temperature during the entire operation process. With air excess coefficients in the interval between the upper and lower concentration limits, reverse currents from the zone of developed combustion successfully cope with this task. When organizing low-temperature combustion near the lean limit, the contribution of reverse currents to heating the fresh gas-air mixture turns out to be insufficient and additional external heating of the components in special heaters with exhaust gases from the turbine is required. The temperature characteristics of the fresh gas-air mixture at the inlet to the chamber and in the zone of return currents, as well as combustion products in the developed flame zone, were obtained from the solution of the energy balance equations. The modes of low-temperature lean combustion with excess air coefficients exceeding the lower concentration limit α = 2 are considered. The calculations were carried out for two values of the ejection coefficient in the zone of reverse currents K = 0.14 and K = 0.30. A K value of 0.14 was obtained using empirical relationships. The value K = 0.30 was obtained from the condition that during stoichiometric combustion, the gas-air mixture is heated completely by reverse currents. It is shown that with an increase in the excess air ratio to ensure a stable position of the flame front, the role of external heating of components increases.


Author(s):  
Simon R. Stow ◽  
Marco Zedda ◽  
Antonios Triantafyllidis ◽  
Andrew Garmory ◽  
Epaminondas Mastorakos ◽  
...  

A Conditional Moment Closure (CMC) approach embedded in an LES CFD framework is presented for simulation of the reactive flow field of an aero-engine combustor operating at altitude relight conditions. Before application to the combustor geometry, the CMC model was validated on the standard lab-scale Sandia flame D. For the combustor simulation, a global mechanism for n-heptane was used along with a Lagrangian approach for the spray, to which a secondary break-up model was applied. The simulation modelled a multi-sector sub-atmospheric rig that was used to verify the altitude relight capability of the combustor. A comprehensive suite of diagnostics was applied to the rig test, including high-speed OH and kerosene PLIF as well as high speed OH* chemiluminescence. The CMC-based CFD simulation was able to predict well the position of the flame front and fuel distribution at the low pressure, low temperature conditions typical of altitude relight. Furthermore, the simulation of the ignition showed strong similarities with OH* chemiluminescence measurements of the event. An EBU-based LES was run too and showed to be unable to capture the flame front as well as the CMC model could. This work demonstrates that CMC LES can be an effective tool to support assessment of the relight capability of aero-engine combustors.


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