A new vortex generator model for use in complex configuration CFD solvers

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  May, N E ^a  

^a Aircraft Research Association Ltd   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; VORTICITY;

AIR JET; CELL TYPES; CFD ANALYSIS; CFD SOLVER; COMPLEX CONFIGURATION; FLAT PLATE; VORTEX GENERATORS;

VORTEX FLOW;

EID: 84987762973     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-2434     Document Type: Conference Paper

References (19)

1. Anderson, B.H., Reddy, D.R., and Kapoor, K., 'A Comparative Study of Full Navier-Stokes and Reduced Navier-Stokes Analyses for Separating Flows within a Diffusing Inlet S-Duct', AIAA-93-2154, 1993.
2. Harloff, G.J., Reichert, B.A., and Wellborn, D.R., 'A Navier-Stokes Analysis and Experimental Data Comparison of Compressible Flow in a Diffusing S-Duct', AIAA-92-2699-CR, 1992.
3. Bray, T.P., 'A Parametric Study of Vane and Air-Jet Vortex Generators', Eng.D. Thesis, Cranfield University College of Aeronautics, Cranfield, UK, 1998.
4. Yu, N.J., Kao, T.J., and Bogue, D.R., 'Computational Simulations of a Commercial Airplane Configuration with Vortex Generators', Proc. Royal Aeronautical Society Aerodynamics Conference, UK, 2000.
5. Currie, T.C., and Syms, J.F., 'Simulation of Flow in a Diffusing S-Duct with and without Air-Jet Vortex Generators', CFD Society of Canada, Montreal, 2000.
6. rd ASME/JSME Joint Fluids Eng. Conf. San Francisco, Calif., USA, 1999.
7. 'Air Intakes for High Speed Vehicles', AGARD-AR-270, 1991.
8. Squire, H.H., 'The Growth of a Vortex in Turbulent Flow', Aeronautical Quarterly, Vol.16, 1965, pp302-306.
9. Wendt, B.J., and Higst, W.R., 'Measurements and Modelling of Flow Structure in the Wake of a Low Profile Wishbone Vortex Generator', AIAA-94-0630, 1994.
10. Shaw, J.A., Peace, A.J., May, N.E., and Pocock, N.F., 'Verification of the CFD Simulation System SAUNA for Complex Configurations', AIAA-94-0393, 1994.
11. st Congress of ICAS, Melbourne, Australia, 1998.
12. Jameson, A., 'A Vertex Based Multi-Grid Algorithm for Three-Dimensional Compressible Flow Calculations', ASME Numerical Methods for Compressible Flow Symposium, 1989.
13. B Jameson, A., Baker, T.J., and Weatherill, N.P., 'Calculation of Inviscid Transonic Flow Over a Complete Aircraft', AIAA-86-0103, 1986.
14. Radespiel, R., 'A Cell-Vertex Multi-Grid Method for the Navier-Stokes Equations', NASA TM101557, 1989.
15. Menter, F.R., 'Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications', AIAA Journal, Vol.32, No.8, ppl598-1605, 1994.
16. Rudy, D., and Strikwerda, J., 'A Non-Reflecting Boundary Condition for Subsonic Navier-Stokes Calculation', J.Comp. Physics, Vol.36, 1980.
17. Anderson, B.H., and Gibb, J., 'Vortex Generator Installation Studies on Steady State and Dynamic Distortion', AIAA-96-3279, 1996.
18. th Int. Symp. On Eng. Turbulence Modelling and Measurements, Eds. Rodi et al., Elsevier, 1999.
19. McGregor, I., and Clark, R., 'A Note on the Calculation of the Rolls Royce Flow Distortion Parameter D9\ RAE TM2086, 1986.