Effect of Diaelectric Barrier Discharge (DBD) Plasma Actuator on Aerodynamics Performance of Vehicle Spoiler
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-3179-6_81
Reference7 articles.
1. Shadmani, S., Mousavi Nainiyan, S.M., Mirzaei, M., Ghasemiasl, R., Pouryoussefi, S.G.: Experimental investigation of flow control over an Ahmed body using DBD plasma actuator. J. Appl. Fluid Mech. 22, 239–252 (2018)
2. Cheng, S.Y., Kwang, Y.C., Shuhaimi, M., Abd Basid, A.R.: Experimental study of yaw angle effect on the aerodynamic characteristics of a road vehicle fitted with a rear spoiler. J. Wind Eng. Ind. Aerodyn. 184, 305–312 (2019)
3. Lou, B., Huang, Z., Ye, S., Wang, G.: Experimental and numerical studies on aerodynamic control of NACA 4418 airfoil with a rotating cylinder. J. Vib. Eng. Tech. 8(1), 141–148 (2019). https://doi.org/10.1007/s42417-019-00085-5
4. Tan, N.D.M.R., Munir, F.A., Tahir, M.M., Herman, S., Mikami, M.: Preliminary investigation of using DBD plasma for application in micro combustors. J. Adv. Res. Fluid Mech. Thermal Sci. 82(1), 105–112 (2021)
5. Shengcheng, J., Bei Z., Jiang, Li., Guangqiu, W.: Numerical study for active flow control using dielectric barrier discharge actuators. J. Aerosp. Eng. 30(5), 04017050–1–04017050–9 (2017)
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