TY - GEN
T1 - The effect of plasma actuator on the depreciation of the aerodynamic drag on box model
AU - Harinaldi, null
AU - Budiarso, null
AU - Julian, James
AU - Rabbani, M. N.
N1 - Publisher Copyright:
© 2016 Author(s).
PY - 2016/6/3
Y1 - 2016/6/3
N2 - Recent active control research advances have provided many benefits some of which in the field of transportation by land, sea as well as by air. Flow engineering by using active control has proven advantages in energy saving significantly. One of the active control equipment that is being developed, especially in the 21st century, is a plasma actuator, with the ability to modify the flow of fluid by the approach of ion particles makes these actuators a very powerful and promising tool. This actuator can be said to be better to the previously active control such as suction, blowing and synthetic jets because it is easier to control, more flexible because it has no moving parts, easy to be manufactured and installed, and consumes a small amount of energy with maximum capability. Plasma actuator itself is the composition of a material composed of copper and a dielectric sheet, where the copper sheets act as an electricity conductor and the dielectric sheet as electricity insulator. Products from the plasma actuators are ion wind which is the result of the suction of free air around the actuator to the plasma zone. This study investigates the ability of plasma actuators in lowering aerodynamic drag which is commonly formed in the models of vehicles by varying the shape of geometry models and the flow speed.
AB - Recent active control research advances have provided many benefits some of which in the field of transportation by land, sea as well as by air. Flow engineering by using active control has proven advantages in energy saving significantly. One of the active control equipment that is being developed, especially in the 21st century, is a plasma actuator, with the ability to modify the flow of fluid by the approach of ion particles makes these actuators a very powerful and promising tool. This actuator can be said to be better to the previously active control such as suction, blowing and synthetic jets because it is easier to control, more flexible because it has no moving parts, easy to be manufactured and installed, and consumes a small amount of energy with maximum capability. Plasma actuator itself is the composition of a material composed of copper and a dielectric sheet, where the copper sheets act as an electricity conductor and the dielectric sheet as electricity insulator. Products from the plasma actuators are ion wind which is the result of the suction of free air around the actuator to the plasma zone. This study investigates the ability of plasma actuators in lowering aerodynamic drag which is commonly formed in the models of vehicles by varying the shape of geometry models and the flow speed.
UR - http://www.scopus.com/inward/record.url?scp=84984551855&partnerID=8YFLogxK
U2 - 10.1063/1.4949292
DO - 10.1063/1.4949292
M3 - Conference contribution
AN - SCOPUS:84984551855
T3 - AIP Conference Proceedings
BT - Proceedings of the 3rd AUN/SEED-NET Regional Conference on Energy Engineering and the 7th International Conference on Thermofluids, RCEnE/THERMOFLUID 2015
A2 - Biwa, Tetsushi
A2 - Kamal, Samsul
A2 - Ohgaki, Hideaki
A2 - Tanimoto, Jun
A2 - Nuthong, Chaiwat
A2 - Widyaparaga, Adhika
A2 - Ishihara, Keiichi N.
A2 - Saptoadi, Harwin
A2 - Sentanuhady, Jayan
A2 - Deendarlianto, null
A2 - Alauddin, Zainal Alimuddin b. Zainal
A2 - Reksowardojo, Iman
A2 - Indarto, null
A2 - Takata, Yasuyuki
A2 - Pranoto, Indro
PB - American Institute of Physics Inc.
T2 - 3rd AUN/SEED-NET Regional Conference on Energy Engineering and the 7th International Conference on Thermofluids, RCEnE/THERMOFLUID 2015
Y2 - 19 November 2015 through 20 November 2015
ER -