TY - JOUR
T1 - On the characteristic flow and flame times for scaling oxy and air flame stabilization modes in premixed swirl combustion
AU - Taamallah, Soufien
AU - Chakroun, Nadim W.
AU - Watanabe, Hirotatsu
AU - Shanbhogue, Santosh J.
AU - Ghoniem, Ahmed F.
N1 - KAUST Repository Item: Exported on 2022-06-07
Acknowledged KAUST grant number(s): KUS-110-010-01
Acknowledgements: This work was supported by the Center For Clean Water and Clean Energy at MIT and KFUPM, under the grant number R12-CE-10 and KAUST under the grant number KUS-110-010-01.
This publication acknowledges KAUST support, but has no KAUST affiliated authors.
PY - 2017/2/7
Y1 - 2017/2/7
N2 - We compare the conditions leading to the stabilization of turbulent methane air and oxy-flames in the outer recirculation zone (ORZ) of a lean premixed acoustically decoupled swirl combustor. The appearance of a flame in the ORZ is an important flame macrostructure transition that was previously shown to be associated with the onset of thermo-acoustic instability under acoustically coupled conditions. We find that, when similar bulk flow conditions are imposed in the ORZ, the transition is governed by the extinction strain rate and can occur at different adiabatic flame temperature and unstretched laminar burning velocity. First, we show that an important non-dimensional parameter characterizing the flow in the ORZ, that is the Strouhal number associated with the azimuthal ORZ spinning frequency, is independent of the Reynolds number and has the same constant value in air and oxy-combustion (St=fORZ.DinUin,bulk≈0.12). This has the important implication that the inlet velocity is a more relevant parameter choice than the inlet Reynolds number in order to maintain similar flow conditions in the ORZ. Next, by comparing the extinction strain rates - computed at the measured ORZ temperature - we show the existence of a single correlation between the inverse of the ORZ spinning frequency (taken as a characteristic ORZ flow time) and the inverse of the extinction strain rate (taken as a characteristic flame time) valid for both air and oxy flames and delimiting the regions of existence of different flame macrostructures.
AB - We compare the conditions leading to the stabilization of turbulent methane air and oxy-flames in the outer recirculation zone (ORZ) of a lean premixed acoustically decoupled swirl combustor. The appearance of a flame in the ORZ is an important flame macrostructure transition that was previously shown to be associated with the onset of thermo-acoustic instability under acoustically coupled conditions. We find that, when similar bulk flow conditions are imposed in the ORZ, the transition is governed by the extinction strain rate and can occur at different adiabatic flame temperature and unstretched laminar burning velocity. First, we show that an important non-dimensional parameter characterizing the flow in the ORZ, that is the Strouhal number associated with the azimuthal ORZ spinning frequency, is independent of the Reynolds number and has the same constant value in air and oxy-combustion (St=fORZ.DinUin,bulk≈0.12). This has the important implication that the inlet velocity is a more relevant parameter choice than the inlet Reynolds number in order to maintain similar flow conditions in the ORZ. Next, by comparing the extinction strain rates - computed at the measured ORZ temperature - we show the existence of a single correlation between the inverse of the ORZ spinning frequency (taken as a characteristic ORZ flow time) and the inverse of the extinction strain rate (taken as a characteristic flame time) valid for both air and oxy flames and delimiting the regions of existence of different flame macrostructures.
UR - http://hdl.handle.net/10754/678626
UR - https://linkinghub.elsevier.com/retrieve/pii/S1540748916302784
UR - http://www.scopus.com/inward/record.url?scp=84997094774&partnerID=8YFLogxK
U2 - 10.1016/j.proci.2016.07.022
DO - 10.1016/j.proci.2016.07.022
M3 - Article
SN - 1873-2704
VL - 36
SP - 3799
EP - 3807
JO - PROCEEDINGS OF THE COMBUSTION INSTITUTE
JF - PROCEEDINGS OF THE COMBUSTION INSTITUTE
IS - 3
ER -