Low reynolds number turbulent flows around a dynamically shaped airfoil

15th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2001, Pages

  Lian, Yongsheng ^a   Steen, Jonas ^b   Trygg Wilander, Marcus ^b   Shyy, Wei ^a  

^a University of Florida   (United States)

^b ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; COMPUTATIONAL FLUID DYNAMICS; FLOW STRUCTURE; REYNOLDS NUMBER; VELOCITY; VORTEX FLOW;

COMPUTATIONAL FRAMEWORK; COMPUTATIONAL INVESTIGATION; COMPUTATIONAL RESULTS; GEOMETRIC CONFIGURATIONS; GEOMETRIC VARIATIONS; LAMINAR TURBULENT TRANSITIONS; MOVING GRID TECHNIQUES; TRANSFINITE INTERPOLATION;

WALL FUNCTION;

EID: 85085780035     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-2723     Document Type: Conference Paper

References (31)

1. Dowell, E.H.(ed.), Crawley, E.F. Jr., Curtiss, H.C., Peters, D.A., Scanlan, R.H., and Sisto, F., A Modern Course in Aeroelasticity, Kluwer Academic Publishers, 1995.
2. Shyy, W., Berg, M., Ljungqvist D., Flapping and Flexible Wings for Biological and Micro Vehicles, Process in Aerospace Sciences, Vol. 35, No. 5, 1999, pp. 455-506.
3. Norberg, U.M., Vertebrate flight: Mechanics, Physiology, Morphology, Ecology and Evolution, New York: Springer, 1990.
4. Liu, H. and Kawachi, K., A Numerical Study of Insect Flight, J. Comput. Phys., Vol. 146, 1998, pp. 124-156.
5. Shyy, W., Klevebring, F., Nilsson, M., Sloan, J., Carroll, B. and Fuentes, C. A Study of Rigid and Flexible Low Reynolds Number Airfoils, Journal of Aircraft, Vol. 36, 1999,pp.523-529.
6. Shyy, W., Jenkins, D.A. and Smith, R.W., Study of Adaptive Shape Airfoils at Low Reynolds Number in Oscillatory Flows, AIAA Journal, Vol. 35, 1997, pp.1545-1548.
7. Shyy, W., Udaykumar, H. S., Rao, M.M and Smith, R.W., Computational Fluid Dynamics with Moving Boundaries, Taylor & Francis, Washington, DC, (1996, revised printing 1997 & 1998) xviii + 285 pages.
8. Fuentes, C., He, X., Carroll, B., Lian, Y.S., and Shyy, W., Low Reynolds Number Flows Around and Airfoil with a Movable Flap-Part 1: Experiments, AIAA Paper 2000-2239, Fluids 2000, June 19-22, 2000.
9. He, X., Fuentes, C., Shyy, W., Lian, Y.S., and Carroll, B., Computation of Transitional Flows around an Airfoil with a Movable Flap, AIAA Paper, 2000-2240, Fluids, 2000, June, 19-22,2000.
10. Guruswamy, G. P., and Byum, C., Fluid-Structural Interactions Using Navier-Stokes Flow Equations Coupled with Shell Finite Element Structures, AIAA Paper 93-3087, July 1993.
11. Byun, C., and Guruswamy, G. A, Comparative Study of Serial and Parallel Aeroelastic Computations of Wings, NASA TM 108805, January. 1994.
12. Smith, M. J., Computational Considerations of an Euler/Navier-Stokes Aeroelastic Method for a Hovering Rotor, Journal of Aircraft, Vol. 33, No. 2, 1996, pp.429-434.
13. Bennett, R. M., and Edwards, J.W., An Overview of Recent Developments in Computational Aeroelasticity, AIAA Paper 98-2421, June 1998.
14. Dowell, E. H., and Hall, K. C., Modeling of Fluid- Structure Interaction, Annu. Rev. Fluid Mech, Vol. 33, 2001, pp.445-490.
15. Lesoinne, M., Farhat, C., Geometric Conservation Laws for Flow Problems with Moving Boundaries and Deformable Meshes, and Their Impact on Aeroelastic Computations, Comput. Meths. AppL Mech. Engrg. Vol. 134, 1996, pp.71-90.
16. Farhat, C., Pierson, K., and Degand, C., CFD Based Simulation of the Unsteady Aeroelastic Response of a Maneuvering Vehicle, AIAA Paper 2000-0899, Jan. 2000.
17. Liu, F., Cai, J., Zhu, Y., Wong, A. S. F., and Tsai, H.M., Calculations of Wing Flutter by a Coupled CFD-CSD Method, AIAA Paper 2000-0907, Jan. 2000.
18. Soulaimani, A., A Finite Element Based Methodology For Computational Nonlinear Aeroelasticity, AIAA Paper 2000-2335, June 2000.
19. Hartwich, P. M., and Agrawal, S., Method for Perturbing Multiblock Patched Grids in Aeroelastic and Design Optimization Applications, AIAA Paper 97-2038, July 1997.
20. Hartwich, P. M., Dobbs, S. K., Arslan, A. E., and Kirn, S. C., Navier-Stokes Computations of Limit Cycle Oscillations for a B-l-like Configuration, AIAA Paper 2000-2338, June 2000.
21. Shyy, W., Thakur, S. S., Ouyang, H., Liu, J. and Blosch, E., Computational Techniques for Complex Transport Phenomena, Cambridge University Press, New York, 1997.
22. Launder, B. E. and Spalding, D. B., The Numerical Computation of Turbulent Flows, Comp. Meth. AppL Mech Engg., Vol. 3, 1974, pp.269-289.
23. Chien, K.-Y., Predictions of Channel and Boundary- Layer flows with a Low-Reynolds-Number Turbulence Model, AIAA Journal, Vol. 20, Jan. 1982, pp. 33-38.
24. He, X., Senocak, I., Shyy, W., Gangadharan, S. N., and Thakur, S. Evaluation of Laminar-Turbulent Transition and Equilibrium near Wall Turbulent Models, Numerical Heat Transfer, Part A, Vol. 37, 2000, pp.101-112.
25. Drela, M. and Giles, M. B., Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils, AIAA Journal, Vol. 25, 1986, pp.1347-1355.
26. Johansen, J. and Sorensen, J. N., Prediction of Laminar/Turbulent Transition in Airfoil Flows, AIAA Paper 98-0702, 1998.
27. Shyy, W., Computational Modeling for Fluid Flow and Interfacial Transport, Elsevier, Amsterdam, The Netherlands, (1994, revised printing 1997) xviii+504 pages.
28. Reuther, J., Jameson, A., Fanner, J., Martinelli, L., and Saunders, D., Aerodynamics Shape Optimization of Complex Aircraft Configurations via an Adjoint Formulation, AIAA Paper 96-0094, Jan. 1996.
29. Robinson, B. A., Batina, J. T., and Yang, H.T.Y., Aeroelastic Analysis of Wings Using the Euler Equations with a Deformaing Mesh, Journal of Aircraft, Vol. 28, No.l 1, Nov. 1991,pp.781-788.
30. Wong, A. S. F., Tsai, H. M., Cai, J., Zhu, Y., and Liu, F., Unsteady Flow Calculations with a Multi-Block Moving Mesh Algorithm, AIAA Paper 2000-1002, Jan. 2000.
31. Eriksson, L. E. Generation of Boundary-Confirming Grids Around Wing-Body Configurations Using Transfinite Interpolation, AIAA Journal, Vol. 20, No. 10, 1982, pp.1313-1320.