TY - GEN
T1 - Experimental study of a nano-second pulse plasma actuator for low reynolds number flow control
AU - Sekimoto, Satoshi
AU - Sulaiman, Taufik
AU - Anyoji, Masayuki
AU - Nonomura, Taku
AU - Fujii, Kozo
PY - 2014
Y1 - 2014
N2 - This paper presents basic characteristics of flow control with a nano-second pulse plasma actuator in low Reynolds number flow. Schlieren visualization in quiescent air verifies that nano-second pulse (NSDBD) actuation can generate compression waves and near-wall flow, whereas burst wave (ACDBD) actuation generates only near-wall flow. The results indicate that strength of a compression wave is independent of pulse repetition frequency. Strength of a compression wave gets stronger with increasing pulse peak voltage because rate of voltage dV0p/dt increase and localized heating is strengthened. Nano-second pulse actuation is applied to leading edge separation control of Re = 63, 000 (free stream flow velocity 10m/s). To understand flow-control characteristics of nano-second pulse actuation, two types of discharge, NSDBD and ACDBD, two types of actuator position, x/c = 0.05 and 0.1, and two types of actuator direction, co-flow blowing and counter-flow blowing, are examined. Generally, flow-control characteristics of NSDBD actuation is very similar to that of ACDBD actuation. With the same voltage amplitude, NSDBD actuation has better control capability than ACDBD actuation. Note that consumption power of NSDBD is 10 to 1000 times larger than that of ACDBD. With an actuator at more downstream position (x/c = 0.1), control capability significantly decreases and separation cannot be suppressed at all. Also results show that NSDBD actuations in counter-flow blowing are worse than those in co-flow blowing for separation suppressing. This indicates that near-wall flow of small momentum from nano-second pulse discharge affects flow-control capability in this Reynolds number condition.
AB - This paper presents basic characteristics of flow control with a nano-second pulse plasma actuator in low Reynolds number flow. Schlieren visualization in quiescent air verifies that nano-second pulse (NSDBD) actuation can generate compression waves and near-wall flow, whereas burst wave (ACDBD) actuation generates only near-wall flow. The results indicate that strength of a compression wave is independent of pulse repetition frequency. Strength of a compression wave gets stronger with increasing pulse peak voltage because rate of voltage dV0p/dt increase and localized heating is strengthened. Nano-second pulse actuation is applied to leading edge separation control of Re = 63, 000 (free stream flow velocity 10m/s). To understand flow-control characteristics of nano-second pulse actuation, two types of discharge, NSDBD and ACDBD, two types of actuator position, x/c = 0.05 and 0.1, and two types of actuator direction, co-flow blowing and counter-flow blowing, are examined. Generally, flow-control characteristics of NSDBD actuation is very similar to that of ACDBD actuation. With the same voltage amplitude, NSDBD actuation has better control capability than ACDBD actuation. Note that consumption power of NSDBD is 10 to 1000 times larger than that of ACDBD. With an actuator at more downstream position (x/c = 0.1), control capability significantly decreases and separation cannot be suppressed at all. Also results show that NSDBD actuations in counter-flow blowing are worse than those in co-flow blowing for separation suppressing. This indicates that near-wall flow of small momentum from nano-second pulse discharge affects flow-control capability in this Reynolds number condition.
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U2 - 10.2514/6.2014-0767
DO - 10.2514/6.2014-0767
M3 - Conference contribution
AN - SCOPUS:85086614018
SN - 9781624102561
T3 - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
BT - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
Y2 - 13 January 2014 through 17 January 2014
ER -