Discrete vortex method for simulating unsteady flow around pitching aerofoils

AIAA Journal

Volumn 35, Issue 3, 1997, Pages 494-499

  Lin, Hequan ^a,b   Vezza, Marco ^a,b   Galbraith, R A McD ^a,b  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

^b Department of Aerospace Engineering ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AEROFOILS; MODELLING-MATHEMATICAL; UNSTEADY FLOW; VORTICITY;

EID: 0030917833     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.122     Document Type: Article

References (9)

1. McCroskey, W. J., "Unsteady Airfoils," Annual Review of Fluid Mechanics, Vol. 14, 1982, pp. 285-311.
2. Carr, L. W., "Progress in Analysis and Production of Dynamic Stall," Journal of Aircraft, Vol. 25, No. 1, 1988, pp. 6-17.
3. Walker, J. M., Helin, H. E., and Strickland, J. H., "An Experimental Investigation of an Airfoil Undergoing Large-Amplitude Pitching Motions," AIAA Journal, Vol. 23, No. 8, 1985, pp. 1141, 1142.
4. Francis, M. S., and Keese, J. E., "Airfoil Dynamic Stall Performance with Large-Amplitude Motions," AIAA Journal, Vol. 23, No. 11, 1985, pp. 1653-1659.
5. Spalart, P. R., "Vortex Method for Separated Flows," NASA TM 100068, June 1988.
6. Chorin, A. J., "Numerical Study of Slightly Viscous Flow," Journal of Fluid Mechanics, Vol. 57, No. 4, 1973, pp. 785-796.
7. Angell, R. K., Musgrove, P. J., and Galbraith, R. A. McD., "Collected Data for Tests on a NACA0015 Aerofoil," Dept. of Aerospace Engineering, Univ. of Glasgow, G. U. Aero Rept. 8803, Glasgow, Scotland, UK, 1988.
8. Vezza, M., "A New Vortex Method for Modelling Two-Dimensional Unsteady Incompressible Viscous Flows" Dept. of Aerospace Engineering, Univ. of Glasgow, G. U. Aero Rept. 9245, Glasgow, Scotland, UK, 1992.
9. Abbott, I. H., and Doenhoff, A. E. V., Theory of Wing Sections, Dover, New York, 1959, Appendix 4.