A correlation indicating incipient dynamic stall

Aeronautical Journal

Volumn 100, Issue 997, 1996, Pages 305-311

  Gracey, M W ^a,b   Niven, A J ^a,c   Coton, F N ^a   Galbraith, R A McD ^a   Jiang, D ^a  

^a UNIVERSITY OF GLASGOW   (United Kingdom)

^b Westland Helicopters Ltd   (United Kingdom)

^c UNIVERSITY OF THE WEST OF SCOTLAND   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; ALGORITHMS; CORRELATION METHODS; REYNOLDS NUMBER; WIND TURBINES;

DYNAMIC STALL; MACH NUMBER; PREDICTIVE ALGORITHM;

AERODYNAMICS;

EID: 0030217596     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (20)

1. CARR, L.W., MCALISTER, K.W. and MCCROSKEY, W.J. Analysis of the development of dynamic stall based on oscillating aerofoil experiments, NASA TND 8382, 1977.
2. MCCROSKEY, W.J., MCALISTER, K.W., CARR, L.W., PUCCI, S.L., LAMBERT, O. and INDERGRAND, R.F. Dynamic stall on advanced airfoil sections, J Am Heli Soc, 1981,13, (1).
3. MCCROSKEY, W.J., CARR, L.W. and MCALISTER, K.W. Dynamic stall experiments on oscillating airfoils, AIAA J, 1976 14, (1).
4. YOUNG, W.H. Fluid mechanics mechanisms in the stall process for helicopters, NASA TM 81956, 1984.
5. GRACEY, M.W. The design and low Mach number wind-tunnel performance of a modified NACA 23012 aerofoil, with an investigation of dynamic stall onset, Ph D Dissertation, Glasgow University Aero Rpt 9108, 1991.
6. SETO, L.Y. GALBRAITH, R.A.McD The effect of pitch rate on the dy'namic stall of a NACA 23012 aerofoil, 11th European Rotorcraft Forum, London, 1985.
7. GALBRAITH, R.A.McD., GRACEY, M.W. LEITCH, E. Summary of pressure data for thirteen aerofoils on the University of Glasgow's aero-foil database, Glasgow University Aero Rpt 9221, 1992.
8. GRACEY, M.W., NIVEN, A.J. and GALBRAITH, R.A.McD. A consideration of low-speed dynamic stall onset, 15th European Rotorcraft Forum, Amsterdam, 1989.
9. SETO, L.Y. An experimental investigation of low speed dynamic stall and reattachment of the NACA 23012 aerofoil under constant pitch motion, Glasgow University Aero Rpt 8829.
10. CARTA, F.O. Analysis of oscillatory pressure data including dynamic stall effects, NASA CR 2394, 1974.
11. SCRUGGS, L.Y., NASH, J.F. and SINGLETON, R.E. Analysis of dynamic stall using unsteady boundary layer theory, NASA CR 2462, 1974.
12. MCALISTER, K.W. and CARR, L.W., Dynamic stall experiments on the NACA 0012 airfoil, NASA TP 1100, 1978.
13. NIVEN, A.J. An experimental investigation into the influence of trailing edge separation on an aerofoil's dynamic stall performance. Glasgow University Aero Rpt 1991, 9107.
14. BEDDOES, T.S. Representation of airfoil behaviour, Vertica, 1983 7, (2).
15. ANGELL, R.K., MUSGROVE, P.J., GALBRAITH, R.A.McD. and GREEN, R.B. Summary of the collected data for tests on the NACA 0015, NACA 0018, NACA 0021, NACA 0025 and NACA 0030, Glasgow University Aero Rpt 9005, 1990.
16. GALBRAITH, R.A.McD., NIVEN, A.J. and COTON, F.N. Unsteady aero-dynamics and its relevance to wind turbines, Wind Eng, 1991 14, (5).
17. COTON, F.N., GALBRAITH, R.A.McD.and JIANG, D. The influence of detailed blade design on the aerodynamic performance of straight bladed vertical axis wind turbines. Journal of Power and Energy, 1996 210, pp. 65-74
18. GALBRAITH, R.A.McD., COTON, F.N. and JIANG, D. The aerodynamic design of vertical axis wind turbines, Glasgow University Aero Rpt 9246.
19. COTON, F.N. and GALBRAITH, R.A.McD. A two-dimensional incompressible aerofoil design package for V.A.W.T. applications, final report for contract AEA/E/5A/CON/5102/1756, Glasgow University Aero Rpt 8904, Sept., 1989.
20. COTON, F.N. and GALBRAITH, R.A.McD. A direct viscid-inviscid interaction scheme for the prediction of two-dimensional aerofoil lift and pitching moment in incompressible flow. Aeronaut J, 1989, 93, (924).