Flow visualization of 3D separation on a plane rectangular wing
Stable case
| ● | Partially tripped flow - Stall cell growth with alpha |
AR 2.0, Re 1.0, a 14.0 tripped at midspan
AR 2.0, Re 1.0, a 13.0 tripped at midspan
AR 2.0, Re 1.0, a 15.0 tripped at midspan
AR 2.0, Re 1.0, a 16.0 tripped at midspan
 |
Bibliography
Bak C., Madsen H.A. and Fuglsang P. Double Stall [Report]. - Roskilde : RISO, 1998.
Barlow J.B., Rae W.H. and Pope A. Low-Speed Wind Tunnel Testing, 3rd Edition [Book]. - [s.l.] : Wiley, 1999 .
Broeren A. and Bragg M. Spanwise Variation in the Unsteady Stalling Flowfields of Two-Dimensional Airfoil Models [Journal] // AIAA JOURNAL. - 2001. - 9 : Vol. 39. - pp. 1451-1461.
Gregory N. [et al.] Progress Report on Observations of Three-Dimensional Flow Patterns obtained during Stall Development on Aerofoils, and on the Problem of Measuring Two-Dimensional Characteristics [Report]. - London : A.R.C.C.P. No. 1146, 1971.
Moss G. F. and Murdin P. M. Two-Dimensional Low-Speed Tunnel Tests on the NACA 0012 Section Including Measurements Made During Pitching Oscillations at the Stall [Report]. - [s.l.] : A.R.C.C.P. No. 1145, 1971.
Mourikis D., Riziotis V. and Voutsinas S. Optimum aerodynamic design of 52 m blade for a prototype 5MW WEC. [Report] : NTUA Technical Report. - Athens : [s.n.], 2005.
Winkelman A E and Barlow J B Flowfield Model for a Rectangular Planform Wing beyond Stall [Journal] // AIAA Journal vol.18 no.8. - 1980. - pp. 1006-1008.
Bak C., Madsen H.A. and Fuglsang P. Double Stall [Report]. - Roskilde : RISO, 1998.
Barlow J.B., Rae W.H. and Pope A. Low-Speed Wind Tunnel Testing, 3rd Edition [Book]. - [s.l.] : Wiley, 1999 .
Broeren A. and Bragg M. Spanwise Variation in the Unsteady Stalling Flowfields of Two-Dimensional Airfoil Models [Journal] // AIAA JOURNAL. - 2001. - 9 : Vol. 39. - pp. 1451-1461.
Gregory N. [et al.] Progress Report on Observations of Three-Dimensional Flow Patterns obtained during Stall Development on Aerofoils, and on the Problem of Measuring Two-Dimensional Characteristics [Report]. - London : A.R.C.C.P. No. 1146, 1971.
Moss G. F. and Murdin P. M. Two-Dimensional Low-Speed Tunnel Tests on the NACA 0012 Section Including Measurements Made During Pitching Oscillations at the Stall [Report]. - [s.l.] : A.R.C.C.P. No. 1145, 1971.
Mourikis D., Riziotis V. and Voutsinas S. Optimum aerodynamic design of 52 m blade for a prototype 5MW WEC. [Report] : NTUA Technical Report. - Athens : [s.n.], 2005.
Winkelman A E and Barlow J B Flowfield Model for a Rectangular Planform Wing beyond Stall [Journal] // AIAA Journal vol.18 no.8. - 1980. - pp. 1006-1008.