Technical Physics Letters
Volumes and Issues
Home » Technical Physics Letters » Year 2022, issue 1 » Article p. 3
>>>
Enhancing the High-lift Properties of a Supercritical Wing by Means of a Modulated Pulse Jet Actuator
Russian version
DOI: 10.21883/TPL.2022.01.52455.18999
Abdolahipour S.1, Mani M.2, Shams Taleghani A.1
1Aerospace Research Institute, Ministry of Science, Research and Technology, Tehran, Iran
2Department of Aerospace Engineering, Amirkabir University of Technology, Tehran, Iran
Email: Arash.taleghani@gmail.com
PDF
In this experimental investigation, a pulse flow control system on a high-lift device of a wing with a NASA SC(2)-0714 airfoil within the Reynolds number range of the take-off and landing phases, is proposed. In this study, an innovative method of signal modulation has been used in order to simultaneously exploit the benefits of both low and high excitation frequencies in one actuator driving signal that are known to be effective in separation control. It is observed that the lift and drag coefficients are improved due to the use of modulated pulse jets compared to the simple pulse jet. Keywords: Flow Control, High-lift configuration, Pulsed jet, Burst modulation, aerodynamic efficiency
  1. A. Salmasi, A. Shadaram, A. Shams Taleghani, IEEE Trans. Plasma Sci., 41 (10), 3079 (2013). DOI: 10.1109/TPS.2013.2280612
  2. M. Mohammadi, A. Shams Taleghani, Arab. J. Sci. Eng., 39 (3), 2363 (2014). DOI: 10.1007/s13369-013-0772-1
  3. M. Sato, K. Okada, K. Asada, H. Aono, T. Nonomura, K. Fujii, Phys. Fluids, 32 (2), 025102 (2020). DOI: 10.1063/1.5136072
  4. .A.V. Voevodin, A.A. Kornyakov, D.A. Petrov, A.S. Petrov, G.G. Sudakov, Tech. Phys. Lett., 44 (8), 687 (2018). DOI: 10.1134/S106378501808014X
  5. K.S. Aley, T.K. Guha, R. Kumar, AIAA J., 58 (5), 2053 (2020). DOI: 10.2514/1.J058939
  6. B. Steinfurth, F. Haucke, AIAA J., 56 (10), 3848 (2018). DOI: 10.2514/1.J057094
  7. C. Cetin, A. Celik, M.M. Yavuz, AIAA J., 56 (1), 90 (2018). DOI: 10.2514/1.J056099
  8. C. Zhuang, G. Yang, Y. Zhu, D. Hu, Renew. Energy, 148, 964 (2020). DOI: 10.1016/j.renene.2019.10.082
  9. A. Saenz-Aguirre, U. Fernandez-Gamiz, E. Zulueta, A. Ulazia, J. Martinez-Rico, Sustainability, 11 (10), 2809 (2019). DOI: 10.3390/su11102809
  10. H.Y. Xu, Q.L. Dong, C.L. Qiao, Z.Y. Ye, Energies, 11 (3), 619 (2018). DOI: 10.3390/en11030619
  11. M. Staats, W. Nitsche, S.J. Steinberg, R. King, CEAS Aeronaut. J., 8 (1), 197 (2017). DOI: 10.1007/s13272-016-0232-1
  12. R. Radespiel, M. Burnazzi, M. Casper, P. Scholz, Aeronaut. J., 120 (1223), 171 (2016). DOI: 10.1017/aer.2015.7
  13. D. Greenblatt, I.J. Wygnanski, Prog. Aerospace Sci., 36 (7), 487 (2000). DOI: 10.1016/S0376-0421(00)00008-7
  14. M.A. Feero, P. Lavoie, P.E. Sullivan, Exp. Fluids, 58 (8), 99 (2017). DOI: 10.1007/s00348-017-2387-x
  15. M. Amitay, A. Glezer, AIAA J., 40 (2), 209 (2002). DOI: 10.2514/2.1662
  16. M. Amitay, D.R. Smith, V. Kibens, D.E. Parekh, A. Glezer, AIAA J., 39 (3), 361 (2001). DOI: 10.2514/2.1323
  17. A. Shams Taleghani, A. Shadaram, M. Mirzaei, S. Abdolahipour, J. Braz. Soc. Mech. Sci. Eng., 40 (4), 173 (2018). DOI: 10.1007/s40430-018-1120-x
  18. M. Mirzaei, A. Shams Taleghani, A. Shadaram, Appl. Mech. Mater., 186, 75 (2012). DOI: 10.4028/www.scientific.net/AMM.186.75
  19. A. Shams Taleghani, A. Shadaram, M. Mirzaei, IEEE Trans. Plasma Sci., 40 (5), 1434 (2012). DOI: 10.1109/TPS.2012.2187683
  20. A. Glezer, Phil. Trans.: Math. Phys. Eng. Sci., 369 (1940), 1476 (2011). http://www.jstor.org/stable/41061602

Подсчитывается количество просмотров абстрактов ("html" на диаграммах) и полных версий статей ("pdf"). Просмотры с одинаковых IP-адресов засчитываются, если происходят с интервалом не менее 2-х часов.

Дата начала обработки статистических данных - 27 января 2016 г.

Publisher:

Ioffe Institute

Institute Officers:

Director: Sergei V. Ivanov

Contact us:

26 Polytekhnicheskaya, Saint Petersburg 194021, Russian Federation
Fax: +7 (812) 297 1017
Phone: +7 (812) 297 2245
E-mail: post@mail.ioffe.ru