Parallel computation of wing flutter with a coupled Navier-Stokes/CSD method

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Sadeghi, M ^a   Yang, S ^a   Liu, F ^a   Tsai, H M ^b  

^a University of California at Irvine   (United States)

^b NATIONAL UNIVERSITY OF SINGAPORE   (Singapore)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; FLUTTER (AERODYNAMICS); TURBULENCE MODELS; VISCOUS FLOW; WINGS;

AEROELASTIC PROBLEMS; ARTIFICIAL DIFFUSION; K-OMEGA TURBULENCE MODEL; NAVIER-STOKES FLOW SOLVER; PARALLEL COMPUTATION; STRUCTURAL DISPLACEMENT; STRUCTURAL EQUATIONS; TEMPORAL DISCRETIZATION;

NAVIER STOKES EQUATIONS;

EID: 85088346389     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1347     Document Type: Conference Paper

References (32)

1. Ballhaus, W. F. and Goorjian, P. M., "Computation of Unsteady Transonic Flows by the Indicial Method, " AIAA Journal, Vol. 16, 1978, pp. 117-124.
2. Isogai, K., "Dip Mechanism of Flutter of a Sweptback Wing: Part II, " AIAA Journal, Vol. 19, 1981, pp. 1240-1242.
3. Borland, C. J. and Rizzetta, D. P., "Nonlinear Transonic Flutter Analysis, " AIAA Journal, Vol. 20, 1982, pp. 1606-1615.
4. Edwards, J., "Transonic Shock Oscillations Calculated with a New Interactive Boundary Layer Coupling Method, " AIAA Paper 93-0777, 1993.
5. Edwards, J., "Transonic Shock Oscillations and Wing Flutter Calculated with an Interactive Boundary Layer Coupling Method, " EUROMECH-Colloquium 349, Simulation of Fluid-Structure Interaction in Aeronautics, Göttingen, Germany, Sept. 1996.
6. Batina, J. T., "A Finite-Difference Approximate-Factorization Algorithm for Solution of the Unsteady Transonic Small-Disturbance Equation, " NASA TP 3129, Jan. 1992.
7. Guruswamy, G. P., "Unsteady Aerodynamic and Aeroelastic Calculations for Wings Using Euler Equations, " AIAA Journal, Vol. 28, 1990, pp. 461-469.
8. Guruswamy, G. P., "Vortical Flow Computations on Swept Flexible Wings Using Navier-Stokes Equations, " AIAA Journal, Vol. 28, 1990, pp. 2077-2084.
9. Sisto, F., Thangam, S., and Abdel-Rahim, A., "Computational Prediction of Stall Flutter in Cascaded Airfoils, " AIAA Journal, Vol. 29, 1991, pp. 1161-1167.
10. Abdel-Rahim, A., Sisto, F., and Thangam, S., "Computational Study of Stall Flutter in Cascaded Airfoils, " Journal of Turbomachinery, Vol. 115, 1993, pp. 157-166.
11. Bakhle, M. A., Reddy, T. S. R., and Jr., T. G. K., "Time Domain Flutter Analysis of Cascades Using a Full-Potential Solver, " AIAA Journal, Vol. 30, 1992, pp. 163-170.
12. Hwang, C. J. and Fang, J. M., "Flutter Analysis of Cascades Using an Euler/Navier-Stokes Solution-Adaptive Approach, " Journal of Propulsion and Power, Vol. 15, 1999, pp. 54-63.
13. Alonso, J. J. and Jameson, A., "Fully-Implicit Time-Marching Aeroelastic Solutions, " AIAA Paper 94-0056, 1994.
14. Sadeghi, M. and Liu, F., "A Method for Calculating Mistuning Effects on Cascade Flutter, " AIAA Journal, Vol. 39, No. 1, 2001.
15. Sadeghi, M. and Liu, F., "Investigation of Mistuning Effects on Cascade Flutter Using a Coupled Method, " AIAA Paper 2002-0952, 2002.
16. Sadeghi, M. and Liu, F., "Investigation of Non-Linear Flutter by a Coupled Aerodynamics and Structural Dynamics Method, " AIAA Paper 2001-0573, 2001.
17. Lee-Rausch, E. and Batina, J. T., "Calculation of Agard Wing 445. 6 Flutter Using Navier-Stokes Aerodynamics, " AIAA Paper 93-3476, 1993.
18. Lee-Rausch, E. and Batina, J. T., "Wing Flutter Boundary Prediction Using Unsteady Euler Aerodynamic Method, " Journal of Aircraft, Vol. 32, 1995, pp. 416-422.
19. Lee-Rausch, E. and Batina, J. T., "Wing Flutter Computations Using an Aerodynamic Model Based on the Navier-Stokes Equations, " Journal of Aircraft, Vol. 33, 1996, pp. 1139-1147.
20. Bendiksen, O. O. and Hwang, G.-Y., "Nonlinear Flutter Calculations for Transonic Wings, " Proceedings of the International Forum on Aeroelasticity and Structural Dynamics, Rome, Italy, June 1997, pp. 105-114.
21. Tsai, H.-M., Wong, A. S. F., Cai, J., Zhu, Y., and Liu, F., "Unsteady Flow Calculations with a Multi-Block Moving Mesh Algorithm, " AIAA Journal, Vol. 39, No. 6, 2001, pp. 1021-1029.
22. Liu, F., Cai, J., Zhu, Y., Tsai, H. M., and Wong, A. S. F., "Calculation of Wing Flutter by a Coupled Fluid-Structure Method, " Journal of Aircraft, Vol. 38, 2001, pp. 334-342.
23. Liu, F. and Zheng, X., "A Strongly-Coupled Time-Marching Method for Solving the Navier-Stokes and k-! Turbulence Model Equations with Multigrid, " J. of Computational Physics, Vol. 128, 1996, pp. 289-300.
24. Liu, F. and Ji, S., "Unsteady Flow Calculations with a Multigrid Navier-Stokes Method, " AIAA Journal, Vol. 34, No. 10, Oct. 1996, pp. 2047-2053.
25. Jameson, A., Schmidt, W., and Turkel, E., "Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes, " AIAA Paper 81-1259, 1981.
26. Schewe, G., Knipfer, A., Mai, H., and Dietz, G., "Experimental and Numerical Investigation of Nonlinear Effects in Transonic Flutter, " DLR IB 232-2002 J 01, 2002.
27. Weber, S., Jones, K. D., Ekaterinaris, J. A., and Platzer, M. F., "Transonic Flutter Computations for a 2D Supercritical Wing, " AIAA Paper 99-0798, 1999.
28. Castro, B. M., Ekaterinaris, J. A., and Platzer, M. F., "Transonic Flutter Computations for the NLR 7301 Airfoil Inside a Wind Tunnel, " AIAA Paper 2000-0984, 2000.
29. Castro, B. M., Jones, K. D., Ekaterinaris, J. A., and Platzer, M. F., "Analysis of the Effect of Porous Wall Interference on Transonic Airfoil Flutter, " AIAA Paper 2001-2725, 2001.
30. Tang, L., Bartels, R. E., Chen, P. C., and Liu, D. D., "Simulation of Transonic Limit Cycle Oscillations Using a CFD Time-Marching Method, " AIAA Paper 2001-1290, 2001.
31. Yates, E. C., Land, N. S., and Foughner, J. T., "Measured and Calculated Subsonic and Transonic Flutter Characteristics of a 45 Sweptback Wing Planform in Air and in Freon-12 in the Langley Transonic Dynamics Tunnel, " AGARD TN D-1616, 1963.
32. "AGARD Standard Aeroelastic Configurations for Dynamic Response I-Wing 445. 6, " NASA TM 100492, Aug. 1987.