Vortex-generator model and its application to flow control

Journal of Aircraft

Volumn 42, Issue 6, 2005, Pages 1486-1491

  Jirásek, Adam ^a,b,c  

^a SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^b Aeronautics Division FFA   (Sweden)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; FLOW CONTROL; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; WINGS;

FLAT PLATES; GENERATOR ARRAYS; VORTEX-GENERATOR MODEL; WING CONFIGURATION;

VORTEX FLOW;

EID: 29544442462     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.12220     Document Type: Article

References (22)

1. Lin, J. C., "Review of Research on Low-Profile Vortex Generators to Control Boundary Layer Separation," Progress in Aerospace Sciences, Vol. 38, Nos. 4-5, 2002, pp. 389-420.
2. Allan, B. G., Yao, C. S., and Lin, J. C., "Numerical Simulation of Vortex Generator Vanes and Jets on a Flat Plate," AIAA Paper 2002-3160, June 2002.
3. Anderson, B. H., Yagle, P. J., Miller, D. N., and Traux, P. P., "A Study of MEMS Flow Control for the Management of Engine Distortion in Compact Inlet Systems," American Society of Mechanical Engineers, FEDSM99-6920, New York, July 1999.
4. Anderson, B. H., and Gibb, J., "Vortex Generator Installation Studies on Steady State and Dynamic Distortion," Journal of Aircraft, Vol. 35, No. 4, 1998, pp. 513-520.
5. Bragg, M. B., and Gregorek, G. M., "Experimental Study of Airfoil Performance with Vortex Generators," Journal of Aircraft, Vol. 24, No. 5, 1987, pp. 305-309.
6. Lin, J. C., Robinson, S. K., McGhee, R. J., and Valerezo, W. O., "Separation Control on High-Lift Airfoils via Micro-Vortex Generators," Journal of Aircraft, Vol. 31, No. 6, 1994, pp. 1317-1323.
7. Yao, C.-S., and Lin, J. C., "Flow-Field Measurement of Device-Induced Embedded Streamwise Vortex on a Flat Plate," AIAA Paper 2002-3162, June 2002.
8. Bore, C. L., "Intakes for Vertical Landing Aircraft," Practical Intake Aerodynamic Design, edited by E. Goldsmith and J. Seddon, AIAA, Washington, DC, 1993, pp. 286-308.
9. May, N. E., "A New Vortex Generator Model for Use in Complex Configuration CFD Solvers," AIAA Paper 2001-31014, June 2001.
10. Kunik, W. G., "Application of a Computational Model for Vortex Generators in Subsonic Internal Flows," AIAA Paper 86-1458, June 1986.
11. Bray, T. P., "A Parametric Study of Vane and Air-Jet Vortex Generators," Engineering Doctorate Thesis, College of Aeronautics, Flow Control and Prediction Group, Cranfield Univ., Shrivenham, U.K., 1998.
12. Wendt, B. J., "Initial Circulation and Peak Vorticity Behavior of Vortices Shed from Airfoil Vortex Generators," NASA/CR-2001-211144, Aug. 2001.
13. Bender, E. E., Anderson, B. H., and Yagle, P. J., "Vortex Generator Modelling for Navier-Stokes Codes," American Society of Mechanical Engineers, FEDSM 99-6919, New York, July 1999.
14. Waithe, K. A., "Source Term Model for an Array of Vortex Generator Vanes," NASA/CR-2003-212157, March 2003.
15. Eliasson, P., "EDGE, a Navier-Stokes Solver for Unstructured Grids," Proceedings to Finite Volumes for Complex Applications III, edited by D. Kroner and R. Herbin, Hermes Penton Science, London, 2002, pp. 527-534, URL: www.Edge.foi.se.
16. Wallin, S., and Johansson, A., "A Complete Explicit Algebraic Reynolds Stress Model for Incompressible and Compressible Turbulent Flows," Journal of Fluid Mechanics, Vol. 403, 2000, pp. 89-132.
17. Advisory Group for Aerospace Research and Development, "Air Intakes for High Speed Vehicles," AGARD, Advisory Rept. 270, Fluid Dynamics Panel Working Group 13, AGARD-AR-270, Sept. 1991.
18. Anderson, B. H., Reddy, D. R., and Kapoor, K., "Study on Computing Separating Flows Within a Diffusion Inlet S-duct," Journal of Propulsion and Power, Vol. 10, No. 5, 1994, pp. 661-667.
19. Aerospace Recommended Practise, "Gas Turbine Engine Inlet Distortion Guidlines," Society of Automotive Engineers, Inc., ARP 1420, Warendale, PA, March 1978.
20. Seddon, J., and Goldsmith, E. L., "Distortion and Swirl," Intake Aerodynamics, 2nd ed., AIAA, Reston, VA, 1985, pp. 269-274.
21. Lin, J. C., "Control of Turbulent Boundary-Layer Separation Using Micro-Vortex Generators," AIAA Paper 98-3404, July 1998.
22. Rae, A. J., Galpin, S. A., and Fulker, J., "Investigation into Scale Effects in the Performance of Sub Boundary-Layer Vortex Generators on Civil Aircraft High-Lift Devices," AIAA Paper 2002-3274, June 2002.