Investigation of slat heel effect on flow field over multi-element aerofoils

Proceedings of the ASME Fluids Engineering Division Summer Meeting

Volumn 1, Issue , 2003, Pages 121-129

  Maddah Sadatieh, S R ^a   Gough, T ^a   Bruun, H H ^a  

^a UNIVERSITY OF BRADFORD   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BOUNDARY LAYERS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; LASER DOPPLER VELOCIMETERS; METAL FOIL; OPTIMIZATION; STRESSES; TURBULENT FLOW; WIND TUNNELS;

REYNOLDS STRESS MODEL (RSM); SIGNAL RECTIFICATION;

FLUID DYNAMICS;

EID: 0348159964     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Alderton J.H and Wilkes N S. Some applications of new finite difference schemes for fluid flow problems. AERE-R 124, 1988.
2. Alemdaroglu N. Experimental investigation of flow around a multielement airfoil. AGARD-CP-515, 1993.
3. Braden J A, Whipkey R R, Jones G S, and Lilley D E Experimental study of the separating confluent boundary layer. NASA CR-3655, 1983; also AIAA paper 86-0505, 1986.
4. Braden J A, Whipkey R R, Jones G S, and Lilley D E Experimental study of the separating confluent boundary layer. NASA CR-3655, 1983; also AIAA paper 86-0505, 1986.
5. Brune G W and Sikavi D A. Experimental investigation of the confluent boundary layer of a multielement low speed airfoil. AIAA paper 83-0566, 1983.
6. st edition, 1995.
7. Clifford-Jones J B. An optimised slat to maximise performance in both aircraft take-off and landing. PhD Thesis, University of Hertfordshire, UK, 1993.
8. Innes F, Pearcey H H and Sykes D M. Improvements in the performance of a three element high lift system by the application of airjet vortex generators. Proc. Conf. High Lift and Separation Control, Royal Aeronautical Society, 1995.
9. Johnston L J. Solution of the Reynolds-averaged Navier-Stokes equations for transonic aerofoil flows. Aeronautical Journal, Oct. 1991, pp. 253-273.
10. Lien F S, Chen W L and Leschziner M A. Computational modelling of high-lift aerofoils with turbulence transport models. Proc. of Conf. High Lift and Separation Control, Royal Aeronautical Society, 1995.
11. Maddah S R Study of the flow field over the multi-element aerofoils, PhD Thesis, Dept. of Mech. and Med. Engineering, Univ. of Bradford, 2000.
12. Mahmood Z, Khan M K, Seal WJ and Braun H H. Comparison of measured and computed velocity fields over a high-lift aerofoil. Proc CMEM, 1995.
13. Mavriplis D J. Euler and Navier-Stokes computations for airfoil geometries using unstructured grids. CASI Journal, Vol. 36, No. 2, pp. 62-71, 1990.
14. Mavriplis D J. Multigrid solution of compressible turbulent flow on unstructured meshes using a two-equation model. AIAA paper 91-0237, Aug. 1991.
15. Moens F and Capbern P. Design and testing of leading-edge high-lift device for laminar flow wing applications. Proc. of Conf. High Lift and Separation Control, Royal Aeronautical Society, 1995.
16. Nakayama A, Kreplin H P and Morgan H L. Experimental investigation of flowfield about a multielement airfoil. AIAA J, Vol. 28, No. 1, pp 14-21, 1990.
17. Nelson T E, Zingg D W, Johnston G W. Compressible Navier-Stokes computations of multielement airfoil flows using multiblock grids. AIAA J, Vol. 32, No. 3, pp506-511, March 1994.
18. Rogers S E, Wiltberger N L and Kwak D. Efficient simulation of incompressible viscous flow over single and multi-element airfoils. AIAA paper 92-0405, Jan. 1992.
19. Savory E, Toy N, Tahouri, and Dalley S. Flow regimes in the cove regions between a slat and wing and between a wing and a flap of a multielement aerofoil. Experimental Thermal and Fluid Sci. 5, pp 307-316, 1992.