TY - GEN
T1 - An investigation on kernel growth variations between conventional spark discharges and nanosecond-pulsed high-frequency discharges
AU - Opacich, Katherine C.
AU - Heyne, Joshua S.
AU - Ombrello, Timothy
AU - Lefkowitz, Joseph K.
AU - Leiweke, Robert J.
AU - Busby, Kenneth
N1 - Publisher Copyright: © 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - Depositing energy using nanosecond-pulsed high-frequency discharges (NPHFD) has been shown to lead to successful fuel-lean ignition. Despite these observations, questions remain regarding how the NPHFD ignition system will perform against the conventional ignition system on shorter timescales and in a flowing environment. This work provides a comparison between the NPHFD ignition system and a conventional, capacitive discharge system in a flowing environment where the total energy deposited, and average power is matched. The results show that matching these characteristics result in similar trends in radius growth, time to minimum growth rate, and radius at which minimum growth rate occurs between the two systems. In utilizing these results as a baseline, it was found that decreasing the average power of the NPHFD system while maintaining the total energy deposited resulted in a ~38% increase in streamwise radius due to advective effects. This larger kernel size comes at the expense of the kernel taking ~20% longer to transition to a self-propagating flame that occurs at a radius that is ~72% larger than the baseline condition. This behavior can be explained by the long duration of the discharge and the low energy density per unit volume in the fluid. Ultimately, the convenience of the larger kernel size comes at the cost of reliability. Therefore, in combustor conditions with strong external quenching physics, depositing the most energy in the shortest time will be optimal in preventing kernel extinction. Conversely, for kernels developing in the presence of mild turbulence, the average power can be decreased, and flow advection can be utilized to grow the kernel over a longer duration without risk of extinction.
AB - Depositing energy using nanosecond-pulsed high-frequency discharges (NPHFD) has been shown to lead to successful fuel-lean ignition. Despite these observations, questions remain regarding how the NPHFD ignition system will perform against the conventional ignition system on shorter timescales and in a flowing environment. This work provides a comparison between the NPHFD ignition system and a conventional, capacitive discharge system in a flowing environment where the total energy deposited, and average power is matched. The results show that matching these characteristics result in similar trends in radius growth, time to minimum growth rate, and radius at which minimum growth rate occurs between the two systems. In utilizing these results as a baseline, it was found that decreasing the average power of the NPHFD system while maintaining the total energy deposited resulted in a ~38% increase in streamwise radius due to advective effects. This larger kernel size comes at the expense of the kernel taking ~20% longer to transition to a self-propagating flame that occurs at a radius that is ~72% larger than the baseline condition. This behavior can be explained by the long duration of the discharge and the low energy density per unit volume in the fluid. Ultimately, the convenience of the larger kernel size comes at the cost of reliability. Therefore, in combustor conditions with strong external quenching physics, depositing the most energy in the shortest time will be optimal in preventing kernel extinction. Conversely, for kernels developing in the presence of mild turbulence, the average power can be decreased, and flow advection can be utilized to grow the kernel over a longer duration without risk of extinction.
UR - http://www.scopus.com/inward/record.url?scp=85092388052&partnerID=8YFLogxK
U2 - 10.2514/6.2020-0428
DO - 10.2514/6.2020-0428
M3 - منشور من مؤتمر
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -