Numerical Investigation on Flow Control of a Hypersonic Airfoil by Plasma Synthetic Jet
Publication: Journal of Aerospace Engineering
Volume 35, Issue 5
Abstract
Plasma synthetic jets (PSJs) have received widespread attention because of their rapid response capability. The use of PSJ shock and thermal effects for active flow control has been investigated in many recent studies. Through numerical simulation, this study found that the geometric position of a PSJ actuator on an airfoil surface is the key factor affecting flow control effects. Different geometric positions have different effects on the lift-drag characteristics of an airfoil, and the flow control mechanism has different components. The flow control mechanism can be divided into three types: the thermal effect, the coupling of the thermal effect and single shock, and the coupling of thermal effect and multiple-shock rebound. The concept of distance provides a reference for determining the geometric arrangement of a PSJ actuator. This study showed that in addition to improving the lift-drag characteristics of an airfoil by reducing drag, directly increasing lift is also a new choice. In addition, in a confirmatory experiment, the nanosecond pulse PSJ actuator pushed the bow shock in a Mach 5 flow; the longest distance was about 1% of the characteristic length of the airfoil.
Practical Applications
In this work, a new type of plasma actuator was used for flow control in hypersonic flow. The influence of the geometric position of the actuator on flow control and the corresponding flow control mechanisms were investigated. This work provide a reference for most work using actuators. For example, the geometric position of an actuator can be selected according to defined in this work and the parameters of the actuator can be set according to the parameter settings of the PSJA. For aerodynamics research, this work provides a new research idea for improving the aerodynamic performance of aircraft. If drag reduction is difficult to achieve, then increasing lift is also a feasible method. For research on plasma flow control, this work broadens its application to hypersonic flow and reveals that a plasma actuator has two flow control effects at the same time. PSJA conducts flow control through the impact effect of the diffracted wave and the mixing effect of the high-temperature cluster; this provides a reference for relevant personnel.
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Data Availability Statement
Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.
References
Anderson, K. V., and D. D. Knight. 2012. “Plasma jet for flight control.” AIAA J. 50 (9): 1855–1872. https://doi.org/10.2514/1.J051309.
Bibi, A., A. Maqsood, S. Sherbaz, and L. Dala. 2017. “Drag reduction of supersonic blunt bodies using opposing jet and nozzle geometric variations.” Aerosp. Sci. Technol. 69 (5): 244–256. https://doi.org/10.1016/j.ast.2017.06.007.
Bletzinger, P., B. N. Ganguly, D. V. Wie, and A. Garscadden. 2005. “Plasmas in high speed aerodynamics.” J. Phys. D Appl. Phys. 38 (4): 33–57. https://doi.org/10.1088/0022-3727/38/4/R01.
Breden, D., and L. Raja. 2012. “Simulations of nanosecond pulsed plasmas in supersonic flows for combustion applications.” AIAA J. 50 (3): 647–658. https://doi.org/10.2514/1.J051238.
Chiatto, M., and L. de Luca. 2017. “Numerical and experimental frequency response of plasma synthetic jet actuators.” In Proc., 55th AIAA Aerospace Sciences Meeting. Reston, VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2017-1884.
Dong, H., X. Geng, Z. Shi, K. Cheng, Y. D. Cui, and B. C. Khoo. 2019. “On evolution of flow structures induced by nanosecond pulse discharge inside a plasma synthetic jet actuator.” Jpn. J. Appl. Phys. 58 (2): 028002. https://doi.org/10.7567/1347-4065/aaf6e5.
Ebrahimi, A., and M. Hajipour. 2018. “Flow separation control over an airfoil using dual excitation of DBD plasma actuators.” Aerosp. Sci. Technol. 79 (34): 658–668. https://doi.org/10.1016/j.ast.2018.06.019.
Emerick, T., M. Y. Ali, C. Foster, F. S. Alvi, and S. Popkin. 2014. “SparkJet characterizations in quiescent and supersonic flowfields.” Exp. Fluids 55 (12): 1858. https://doi.org/10.1007/s00348-014-1858-6.
Falempin, F., A. A. Firsov, D. A. Yarantsev, M. A. Goldfeld, K. Timofeev, and S. B. Leonov. 2015. “Plasma control of shock wave configuration in off-design mode of inlet.” Exp. Fluids 56 (3): 54–64. https://doi.org/10.1007/s00348-015-1928-4.
Geng, X., W. Zhang, Z. Shi, Z. Li, Q. Sun, and Z. Sun. 2021. “Experimental study on frequency characteristics of the actuations produced by plasma synthetic jet actuator and its geometric effects.” Phys. Fluids 33 (6): 067113. https://doi.org/10.1063/5.0048300.
Golbabaei-Asl, M., D. Knight, and S. Wilkinson. 2015. “Novel technique to determine sparkjet efficiency.” AIAA J. 53 (2): 501–504. https://doi.org/10.2514/1.J053034.
Haack Popkin, S., B. Cybyk, B. Land, C. Foster, T. Emerick, and F. Alvi. 2013. “Recent performance-based advances in sparkjet actuator design for supersonic flow applications.” In Proc., 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, VA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2013-322.
Huang, W., L. Yan, J. Liu, L. Jin, and J.-G. Tan. 2015. “Drag and heat reduction mechanism in the combinational opposing jet and acoustic cavity concept for hypersonic vehicles.” Aerosp. Sci. Technol. 42 (56): 407–414. https://doi.org/10.1016/j.ast.2015.01.029.
Jin, D., W. Cui, Y. Li, F. Li, M. Jia, Q. Sun, and B. Zhang. 2015. “Characteristics of pulsed plasma synthetic jet and its control effect on supersonic flow.” Chin. J. Aeronaut. 28 (1): 66–76. https://doi.org/10.1016/j.cja.2014.12.012.
Knight, D. 2008. “Survey of aerodynamic drag reduction at high speed by energy deposition.” J. Propul. Power 24 (6): 1153–1167. https://doi.org/10.2514/1.24595.
Kossyi, I. A., A. Y. Kostinsky, A. A. Matveyev, and V. P. Silakov. 1992. “Kinetic scheme of the non-equilibrium discharge in nitrogen-oxygen mixtures.” Plasma Sources Sci. Technol. 1 (8): 207–220. https://doi.org/10.1088/0963-0252/1/3/011.
Li, S.-B., T.-T. Zhang, C. Ou, W. Huang, and J. Chen. 2020. “Mechanism study on drag reduction and thermal protection for the porous opposing jet in hypersonic flow.” Aerosp. Sci. Technol. 103 (5): 105933. https://doi.org/10.1016/j.ast.2020.105933.
Li, Z., Z. Shi, and H. Du. 2017. “Analytical model: Characteristics of nanosecond pulsed plasma synthetic jet actuator in multiple-pulsed mode.” Adv. Appl. Math. Mech. 9 (2): 439–462. https://doi.org/10.4208/aamm.2015.m1297.
Minesi, N., S. Stepanyan, P. Mariotto, G. D. Stancu, and C. O. Laux. 2020. “Fully ionized nanosecond discharges in air: The thermal spark.” Plasma Sources Sci. Technol. 29 (8): 085003. https://doi.org/10.1088/1361-6595/ab94d3.
Mintoussov, E. I., S. J. Pendleton, F. G. Gerbault, N. A. Popov, and S. M. Starikovskaia. 2011. “Fast gas heating in nitrogen–oxygen discharge plasma: II. Energy exchange in the afterglow of a volume nanosecond discharge at moderate pressures.” J. Phys. D Appl. Phys. 44 (28): 285202. https://doi.org/10.1088/0022-3727/44/28/285202.
Narayanaswamy, V., L. L. Raja, and N. T. Clemens. 2010. “Characterization of a high-frequency pulsed-plasma jet actuator for supersonic flow control.” AIAA J. 48 (2): 297–305. https://doi.org/10.2514/1.41352.
Narayanaswamy, V., L. L. Raja, and N. T. Clemens. 2012. “Control of unsteadiness of a shock wave/turbulent boundary layer interaction by using a pulsed-plasma-jet actuator.” Phys. Fluids 24 (7): 076101. https://doi.org/10.1063/1.4731292.
Poggie, J., I. Adamovich, N. Bisek, and M. Nishihara. 2012. “Numerical simulation of nanosecond-pulse electrical discharges.” Plasma Sources Sci. Technol. 22 (1): 015001. https://doi.org/10.1088/0963-0252/22/1/015001.
Popov, N. A. 2011. “Fast gas heating in a nitrogen–oxygen discharge plasma: I. Kinetic mechanism.” J. Phys. D Appl. Phys. 44 (28): 285201. https://doi.org/10.1088/0022-3727/44/28/285201.
Reedy, T. M., N. V. Kale, J. C. Dutton, and G. S. Elliott. 2013. “Experimental characterization of a pulsed plasma jet.” AIAA J. 51 (8): 2027–2031. https://doi.org/10.2514/1.J052022.
Rong, Y., Y. Wei, and R. Zhan. 2016. “Research on thermal protection by opposing jet and transpiration for high speed vehicle.” Aerosp. Sci. Technol. 48 (23): 322–327. https://doi.org/10.1016/j.ast.2015.11.014.
Sary, G., G. Dufour, F. Rogier, and K. Kourtzanidis. 2014. “Modeling and parametric study of a plasma synthetic jet for flow control.” AIAA J. 52 (8): 1591–1603. https://doi.org/10.2514/1.J052521.
Shang, J. S. 2002. “Plasma injection for hypersonic blunt-body drag reduction.” AIAA J. 40 (6): 1178–1186. https://doi.org/10.2514/2.1769.
Starikovskii, A. Y., A. A. Nikipelov, M. M. Nudnova, and D. V. Roupassov. 2009. “SDBD plasma actuator with nanosecond pulse-periodic discharge.” Plasma Sources Sci. Technol. 18 (3): 034015. https://doi.org/10.1088/0963-0252/18/3/034015.
Wang, J.-J., K.-S. Choi, L.-H. Feng, T. N. Jukes, and R. D. Whalley. 2013. “Recent developments in DBD plasma flow control.” Prog. Aerosp. Sci. 62 (May): 52–78. https://doi.org/10.1016/j.paerosci.2013.05.003.
Wang, L., Z.-X. Xia, Z.-B. Luo, and J. Chen. 2014. “Three-electrode plasma synthetic jet actuator for high-speed flow control.” AIAA J. 52 (4): 879–882. https://doi.org/10.2514/1.J052686.
Zhang, H., Y. Wu, Y. Li, X. Yu, and B. Liu. 2019. “Control of compressor tip leakage flow using plasma actuation.” Aerosp. Sci. Technol. 86 (1): 244–255. https://doi.org/10.1016/j.ast.2019.01.009.
Zhang, W., X. Geng, Z. Shi, and S. Jin. 2020. “Study on inner characteristics of plasma synthetic jet actuator and geometric effects.” Aerosp. Sci. Technol. 105 (10): 106044. https://doi.org/10.1016/j.ast.2020.106044.
Zong, H., M. Chiatto, M. Kotsonis, and L. de Luca. 2018. “Plasma synthetic jet actuators for active flow control.” Actuators 7 (4): 77. https://doi.org/10.3390/act7040077.
Zong, H., and M. Kotsonis. 2017. “Formation, evolution and scaling of plasma synthetic jets.” J. Fluid Mech. 837 (2): 147–181. https://doi.org/10.1017/jfm.2017.855.
Zong, H., Y. Wu, H. Song, and M. Jia. 2016. “Efficiency characteristic of plasma synthetic jet actuator driven by pulsed direct-current discharge.” AIAA J. 54 (11): 3409–3420. https://doi.org/10.2514/1.J054987.
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Published In
Journal of Aerospace Engineering
Volume 35 • Issue 5 • September 2022
Copyright
© 2022 American Society of Civil Engineers.
History
Received: Jan 21, 2022
Accepted: Apr 28, 2022
Published online: Jun 30, 2022
Published in print: Sep 1, 2022
Discussion open until: Nov 30, 2022
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