TY - GEN
T1 - Numerical study of a nsdbd actuator
T2 - AIAA Aerospace Sciences Meeting, 2018
AU - Zhu, Yifei
AU - Shcherbanev, Sergey A.
AU - Starikovskaia, Svetlana M.
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018/1/1
Y1 - 2018/1/1
N2 - nSDBD (nanosecond surface dielectric barrier discharges) have a wide range of applications in the domain of aerodynamics. Numerical simulations were conducted to investigate the dynamics of discharge, the spatial and temporal structures of streamers, the production of active species, and energy deposition. A 2D plasma-fluid coupling code was specially designed and validated by previous experiments to study the discharge parameters and fluid responses in SDBD. The calculations agree well with available experiments and provide direct insights into the evolution of streamers and give a physical spatio-temporal description of fast gas heating energy for further high resolution computational fluid dynamics simulations. The calculations were conducted under P=1 bar, T=300 K condition, with an applied voltage of 24kV for both positive and negative polarities. Active species production in the streamer channel was analysed, the energy deposited into fluid was obtained. Results show the difference between distributions of charged species and excited species, the different mechanisms of discharges under positive and negative polarities leading to different distributions of energy release, and thus different fluid response characteristics.
AB - nSDBD (nanosecond surface dielectric barrier discharges) have a wide range of applications in the domain of aerodynamics. Numerical simulations were conducted to investigate the dynamics of discharge, the spatial and temporal structures of streamers, the production of active species, and energy deposition. A 2D plasma-fluid coupling code was specially designed and validated by previous experiments to study the discharge parameters and fluid responses in SDBD. The calculations agree well with available experiments and provide direct insights into the evolution of streamers and give a physical spatio-temporal description of fast gas heating energy for further high resolution computational fluid dynamics simulations. The calculations were conducted under P=1 bar, T=300 K condition, with an applied voltage of 24kV for both positive and negative polarities. Active species production in the streamer channel was analysed, the energy deposited into fluid was obtained. Results show the difference between distributions of charged species and excited species, the different mechanisms of discharges under positive and negative polarities leading to different distributions of energy release, and thus different fluid response characteristics.
UR - https://www.scopus.com/pages/publications/85141651990
U2 - 10.2514/6.2018-2046
DO - 10.2514/6.2018-2046
M3 - Conference contribution
AN - SCOPUS:85141651990
SN - 9781624105241
T3 - AIAA Aerospace Sciences Meeting, 2018
BT - AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
Y2 - 8 January 2018 through 12 January 2018
ER -