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The effects of trailing edge blowing on aerodynamic characteristics of the NACA 0012 airfoil and optimization of the blowing slot geometry

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Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The effects of blowing and its parameters including the jet amplitude, blowing coefficient and jet width in order to flow control was evaluated for a NACA 0012 airfoil. The flow was considered as fully turbulent with the Reynolds number of 5 · 105, and the Menter shear stress turbulent model was employed. Tangential and perpendicular blowing at the trailing edge were applied on the airfoil upper surface, and the jet widths were varied from 1.5 to 4 percent of the chord length, and the jet amplitude was also selected 0.1, 0.3 and 0.5. In the tangential blowing, the results showed that when the blowing amplitude increases, the lift- to-drag ratio rises by 15 percent, however, the smaller amounts of the blowing amplitude are more effective in the perpendicular blowing. Furthermore, when the blowing jet width rises, the lift-to-drag ratio increases continuously in the tangential blowing and decreases quasi- linear in the perpendicular blowing. In this study, the blowing jet width 3.5 and 4 percent of the chord length for the tangential blowing was selected as optimal values as well as smaller amounts of blowing jet width are more suitable for the perpendicular blowing. Finally, the lift-to-drag ratio was increased by 17 percent for the tangential blowing in the angle of attack of 18 degrees.
Rocznik
Strony
165--179
Opis fizyczny
Bibliogr. 29 poz., rys., tab.
Twórcy
autor
  • Islamic Azad University, Mashhad Branch, Department of Mechanical Engineering, Mashhad, Iran
autor
  • Islamic Azad University, Mashhad Branch, Department of Mechanical Engineering, Mashhad, Iran
Bibliografia
  • 1. Abbott I.H., Von Doenhoff A.E., 1959, Theory of Wing Sections, Dover Publications, New York
  • 2. Critzos C.C., Heyson H.H., Boswinkle W., 1955, Aerodynamics characteristics of NACA 0012 airfoil section at angle of attacks from 0◦ to 180◦, NACA TN, 3361
  • 3. Dirlik S., Kimmel K., Sekelsky A., Slomski J., 1992, Experimental evaluation of a 50-percent thick airfoil with blowing and suction boundary layer control, AIAA Paper, 92, 427-445
  • 4. Eppler R., 1990, Airfoil Design and Data, Springer, Berlin
  • 5. Flatt J., 1961, The history of boundary layer control research in the United States of America, [In:] Boundary Layer and Flow Control: its Principles and Application, G.V. Lachmann (Edit.), New York, Pergamon Press
  • 6. Gad-el-hak M., 2000, Control Flow: Passive, Active and Reactive Flow Management, Cambridge University Press, United Kingdom, 25-35
  • 7. Genc M.S., Keynak U., Yapici H., 2011, Performance of transition model for predicting low Re aerofoil flows without/with single and simultaneous blowing and suction, European Journal of Mechanics B/Fluids, 30, 2, 218-235
  • 8. Glauert M.B., 1947, The application of the exact method of aerofoil design,Aeronautical Research Council, R&M, 2683
  • 9. Goodarzi M., Fereidouni R., Rahimi M., 2012, Investigation of flow control over a NACA 0012 airfoil by suction effect on aerodynamic characteristics, Canadian Journal of Mechanical Sciences and Engineering, 3, 3, 102-108
  • 10. Guowei Y., Shanwu W., Ningyu L., Lixian Z., 1997, Control of unsteady vertical lift on an airfoil by leading-edge blowing suction, ACTA Mechanica Sinica (English Series), 13, 4, 304-312
  • 11. Hazen D.C., 1967, Boundary layer control, Journal of Fluid Mechanics, 29, 200-208
  • 12. Huang L., Huang P.G., LeBeau R.P., 2004, Numerical study of blowing and suction control mechanism on NACA 0012 airfoil, Journal of Aircraft, 41, 5, 1005-1013
  • 13. Jacobs E., Sherman A., 1937, Airfoil section characteristics as affected by variations of the Reynolds number, NACA Report, 586, 227-264
  • 14. Jensch C., Pfingsten, K.C., Radespiel, R., 2010, Numerical investigation of leading edge blowing and optimization of the slot geometry for a circulation control airfoil, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 112, 183-190
  • 15. Mashud M., Hossain F., 2010, Experimental study of flow separation control of an airfoil by suction and injection, 13th Asian Congress of Fluid Mechanics, 166-169
  • 16. Menter, F.R., Kuntz, M., Langtry, R., 2003, Ten years of industrial experience with the SST turbulence model, 4th International Symposium on Turbulence, Heat and Mass Transfer, Turkey
  • 17. Nae C., 1998, Synthetics jets influence on NACA 0012 airfoil at high angle of attacks, AIAA Papers, 98-4523
  • 18. Olejniczak J., Lyrintzis A.S., 1994, Design of optimized airfoils in subcritical flow, Journal of Aircraft, 31, 3, 680-687
  • 19. Ravindran S.S., 1999, Active control of flow separation over an airfoil, Report of Langley Research Center, TM-1999-209838
  • 20. Rizzetta D.P., Visbal M.R., Stank M.J., 1999, Numerical investigation of synthetic jet flow fields, AIAA Journal, 37, 8, 919-927
  • 21. Rosas C.R., 2005, Numerical simulation of flow separation control by oscillatory fluid injection, Ph.D. Thesis, A&M University, Texas
  • 22. Sahu R., Patnaik B.S.V., 2011, CFD simulation of momentum injection control past a stream-lined body, International Journal of Numerical Methods for Heat and Fluid Flow, 21, 8, 960-1001
  • 23. Schlichting H., 1968, Boundary Layer Theory, McGraw-Hill, New York, 347-362
  • 24. Seifert A., Darabi A., Wygnansky I., 1996, Delay of airfoil stall by periodic extinction, Journal of Aircraft, 33, 4, 691-698
  • 25. Sheldhal R.E., Klimas P.C., 1981, Aerodynamic characteristics of seven airfoil sections through 180 degrees angle of attack for use in aerodynamic analysis of vertical axis wind tunnel, Sandia National Laboratories Report, SAND80-2114
  • 26. You D., Moin P., 2008, Active control of flow separation over an airfoil using synthetic jets, Journal of Fluids and Structures, 24, 8, 1349-1357
  • 27. Yousefi K., Saleh R., Zahedi P., 2012, Investigation for increase or decrease the lift and drag coefficient on the airfoil with suction and blowing, International Conference on Mechanical Engineering and Advanced Technology, Iran
  • 28. Yousefi K., Saleh R., Zahedi P., 2013a, Numerical investigation of suction and length of suction jet on aerodynamic characteristics of the NACA 0012 airfoil, International Journal of Materials, Mechanics and Manufacturing, 1, 2, 136-142
  • 29. Yousefi K., Saleh R., Zahedi P., 2013b, Numerical study of flow separation control by tangential and perpendicular blowing on the NACA 0012 airfoil, International Journal of Engineering, 7, 1, 10-24
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a655a1af-1707-4339-b6ef-5ab3be26e703
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