Acceso abierto

Effects of Boundary Layer Control Method on Hydrodynamic Characteristics and Tip Vortex Creation of a Hydrofoil


Cite

1. Kroo, I. : Non-planar wings concepts for increases aircraft efficiency. VKI lecture series on Innovative Configurations and Advanced Concepts for Future Civil Aircraft, 2005.Search in Google Scholar

2. Park, K., Lee J. Influence of endplate on aerodynamic characteristics of low-aspect ratio wing in ground effect. J. Mech. Sci. Tech., 22, 2578-2589, 2008.10.1007/s12206-008-0805-ySearch in Google Scholar

3. Kaplan S.M., Altman A. : Wake Vortices Measurements for Low Aspect Ratio Wings at Low Reynolds Number. J. Aircraft. 44, 1631-1639, 2007.10.2514/1.23096Search in Google Scholar

4. Mansour, N.N. : Numerical Simulation of the Tip Vortex of a Low Aspect Ratio Wing at Transonic Speed. AIAA, 23, 1143-1149, 1985.10.2514/3.9056Search in Google Scholar

5. McAlister, K.W., Takashi T.K. : NACA 0015 Wing Pressure and Trailing Vortex Measurements. ACSOM Technical Report 91-A-003, California, 1991.Search in Google Scholar

6. Mariani, J., Zilliac G., Chow J., Bradshaw P. : Numerical/ Experimental Study of a Wingtip Vortex in the Near Field. AIAA, 33. 1561-1568, 1995.Search in Google Scholar

7. Englar, R.J. : Circulation control for high lift and drag generation on STOL aircraft. . J. Aircraft, 12, 457-463, 1975.10.2514/3.59824Search in Google Scholar

8. Englar, R.J. Trabouh, L.A., Hemmersly R. : STOL potential of the circulation control wing for high-performance aircraft. J. Aircraft, 25, 236-243, 1978.Search in Google Scholar

9. Wood, N. Nielsen J.: Circulation control airfoils-past, present, future. AIAA. 85-0204, 23rd Aerospace Sciences Meeting, Reno, Nevada, 1985.10.2514/6.1985-204Search in Google Scholar

10. Wood, N. and Robert, L. : Control of vortical lift on Delta wings by tangential leading-edge blowing. J. Aircraft, 25, 236-243, 1988.10.2514/3.45583Search in Google Scholar

11. Wood, N., Robert, L. and Celik Z. : Control of asymmetric vertical flows over delta wings at high angle of attack. J. Aircraft. 27, 429-435, 1990.10.2514/3.25294Search in Google Scholar

12. Modi, V. Fernando, M. Yokomizo, T. : Drag reduction of bluff bodies through moving surface boundary layer control. AIAA Paper No. 1990-298, 28th Aerospace Sciences Meeting, Reno, Nevada, 1990.Search in Google Scholar

13. Johari, H. and MaManus, K. : Visualization of pulsed vortex generator jets for active control of boundary layer separation. AIAA Paper 1997-2021, 28th Fluid Dynamic Conference, Snowmass Village, Colorado, 1997.10.2514/6.1997-2021Search in Google Scholar

14. McManus, K. Magill, J. : Airfoil performance enhancement using pulsed jet separation control. AIAA Paper 1997-1971, 4th Shear Flow Control Conference, Snowmass Village, Colorado, June 29-July 2, 1997.10.2514/6.1997-1971Search in Google Scholar

15. Zha G, Paxton C. : A novel airfoil circulation augment flow control method using co-flow jet. AIAA Paper 2004-2208, 2nd AIAA Flow Control Conference, Portland, Oregon, 2004.10.2514/6.2004-2208Search in Google Scholar

16. Zha, G., Carrol, B., Paxton, C., Conely C., Wells, A. : High Performance Airfoil Using Co-Flow Jet Flow Control. AIAA Paper 2005-1260, 43rd Aerospace Sciences Meeting, Reno, Nevada, 2005.10.2514/6.2005-1260Search in Google Scholar

17. Gilarranz, J.L., Traun. L.W., Radiniotis. O.K. : A new class of synthetic jet actuators-part 1: design, fabrication and bench top characterization. J. Fluids Eng. 127, 367-376, 2005.10.1115/1.1839931Search in Google Scholar

18. Gilarranz, J.L., Traun. L.W., Radiniotis. O.K. : A new class of synthetic jet actuators-part 2: Application to flow separation control. J. Fluids Eng. 127, 377-387, 2005.10.1115/1.1882393Search in Google Scholar

19. You, D., Moin, P. : Active control of flow separation over an airfoil using synthetic jets. J. Fluids Struct. 24, 1349-1357, 2008.10.1016/j.jfluidstructs.2008.06.017Search in Google Scholar

20. Agrawal, G., Rediniotis, O.K., Taub, L.W. : An experimental investigation on the effects of pulsed air blowing separation control on NACA 0015. 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV. AIAA Journal, 0, 1-12, 2005. ?Search in Google Scholar

21. Mack, S. Berhm, C., Heine B., Kurz, A., Fasel, H. F. : Experimental investigation of separation and separation control on a laminar airfoil. 4th AIAA Flow Control Conference. Seattle, WA, 2008.10.2514/6.2008-3766Search in Google Scholar

22. Gompertz, K. Bones, J.P. : Combined unsteady wakes and active flow control on a low-pressure turbine airfoil. J. Prop. Power, 5, 990-1000, 2011.10.2514/1.B34032Search in Google Scholar

23. Packard, N. O. Thakejr, M. P., Bonilla, C. H., Gompertz, K, Bones, J. : Active control of flow separation on a laminar aircraft. AIAA Journal. 51, (5), 1032-1041, 2013.10.2514/1.J051556Search in Google Scholar

24. Gardner, A.D., Ritchter, K., Neuhaus, D. Experimental investigation of high-pressure pulsed blowing for dynamic stall control, CAES Aeronautical J, 5, 185-198, 2014.10.1007/s13272-014-0099-ySearch in Google Scholar

25. Zhang, W., Samataney, R. A. : Direct numerical simulation investigation of the synthetic jet frequency effects on separation control of low-Re flow past an airfoil. Physics of Fluids, 27, 055101, 2015.Search in Google Scholar

26. Mang, X., Yan, X., Hu, H., Liu, F., Luo, S. : Plasma laminar- separation-bubble control over airfoil at low Reynolds numbers. 46th AIAA Plasmadynamics and Lasers Conference, 2015.10.2514/6.2015-2954Search in Google Scholar

27. Hipp, K.D., Walker, M., Benton, S.I., Bones, J. : Control of leading-edge airfoil stall using pulsed jets. 54th AIAA Aerospace Sciences Meeting, 2016.10.2514/6.2016-1822Search in Google Scholar

28. Bernardini, C., Beneton S. I., Hipp, K. D., Bons, J. P. : Large low-frequency oscillations initiated by flow control on a poststall airfoil, ? 2016.10.2514/1.J054321Search in Google Scholar

29. Ghadimi, P., Kermani, S., Feizi Chakab, M.A. : Numerical hydro-acoustic analysis of NACA foils in marine applications and comparison of their acoustic behavior. ISRN Mech. Eng., 2013, 1-12, 2013.10.1155/2013/714363Search in Google Scholar

30. Kelterer ME, Pecnik R, Sanz W. : Computation of Laminar-Turbulent Transition in Turbumachinery Using the Correlation Based γ-Reθ Transition Model. ASME Proceedings, Turbomachinery, 7, 613-622.Search in Google Scholar

31. Counsil J.N., Boulama K.G. 2013? : Low-Reynolds-Number Aerodynamic Performances of the NACA 0012 and Selig-Donovan 7003 Airfoils. J Aircraft, 50(1), 204-216. 201010.2514/1.C031856Search in Google Scholar

32. Khayatzadeh P. , Nadarajah S. : Aerodynamic Shape Optimization via Discrete Viscous Adjoint Equations for the k-wSST Turbulence and y-Re0 Transition Models. In: 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, US. 2011.10.2514/6.2011-1247Search in Google Scholar

33. Menter, F.R. : Two equation eddy-viscosity turbulence models for aerodynamics for engineering applications. AIAA J. 32(8). 1598-1605. 1994.10.2514/3.12149Search in Google Scholar

34. Ansys CFX User’s Manual 2013. 34. McCormick, D. : Boundary Layer Separation Control With Directed Synthetic Jets. AIAA Paper No. 2000-0519, 2011.Search in Google Scholar

eISSN:
2083-7429
Idioma:
Inglés
Calendario de la edición:
4 veces al año
Temas de la revista:
Engineering, Introductions and Overviews, other, Geosciences, Atmospheric Science and Climatology, Life Sciences