TY - GEN
T1 - Study of Non-Equilibrium Plasma Effects on Detonation in Fuel Lean Natural Gas Mixtures
AU - Talukdar, Shaon
AU - Hossain, Md Monir
AU - Ranganathan, Rajagopalan V.
AU - Uddi, Mruthunjaya
N1 - Publisher Copyright:
© 2021 IEEE.
PY - 2021/9/12
Y1 - 2021/9/12
N2 - Combustion can occur with flame propagations at both subsonic and supersonic velocities, known as deflagration and detonation, respectively. In detonation, the hot gases of combustion are expelled at supersonic velocities, generating thrust. Combustors designed for utilizing this type of combustion, like Rotating Detonation Combustors (RDCs), are found to be more efficient (by 4-5%) than in the traditional constant pressure gas turbine combustors.
AB - Combustion can occur with flame propagations at both subsonic and supersonic velocities, known as deflagration and detonation, respectively. In detonation, the hot gases of combustion are expelled at supersonic velocities, generating thrust. Combustors designed for utilizing this type of combustion, like Rotating Detonation Combustors (RDCs), are found to be more efficient (by 4-5%) than in the traditional constant pressure gas turbine combustors.
UR - https://www.scopus.com/pages/publications/85119583939
U2 - 10.1109/ICOPS36761.2021.9588370
DO - 10.1109/ICOPS36761.2021.9588370
M3 - Conference contribution
AN - SCOPUS:85119583939
T3 - IEEE International Conference on Plasma Science
BT - 2021 IEEE International Conference on Plasma Science, ICOPS 2021
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2021 IEEE International Conference on Plasma Science, ICOPS 2021
Y2 - 12 September 2021 through 16 September 2021
ER -