TY - GEN
T1 - Effect of inlet disturbances on bluff body stabilized combustion
AU - Madanmohan, M.
AU - Pandey, S.
AU - Kushari, A.
PY - 2008/12/1
Y1 - 2008/12/1
N2 - Combustion instability is a type of thermo-acoustic oscillation that can be detrimental for combustion system leading to even flame out. This paper deals with the effect of inlet disturbances on the stability of bluff body stabilized flames and identifies the influence of vortex formation at the bluff body as the principle cause for the onset of oscillations in otherwise stable flame. It also points to the fact that the combustion dynamics can be affected by the inlet flow modulation, which can be used to suppress combustion instability through controlled, phase locked perturbations in the incoming flow.
AB - Combustion instability is a type of thermo-acoustic oscillation that can be detrimental for combustion system leading to even flame out. This paper deals with the effect of inlet disturbances on the stability of bluff body stabilized flames and identifies the influence of vortex formation at the bluff body as the principle cause for the onset of oscillations in otherwise stable flame. It also points to the fact that the combustion dynamics can be affected by the inlet flow modulation, which can be used to suppress combustion instability through controlled, phase locked perturbations in the incoming flow.
UR - http://www.scopus.com/inward/record.url?scp=77957845980&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:77957845980
SN - 9781563479434
T3 - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
BT - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
T2 - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Y2 - 21 July 2008 through 23 July 2008
ER -