Numerical simulation of flow induced vibration based on fully coupled fluid-structural interactions

34th AIAA Fluid Dynamics Conference and Exhibit

Volumn , Issue , 2004, Pages

  Chen, Xiangying ^a   Zha, Ge Cheng ^a   Hu, Zongjun ^a  

^a University of Miami College of Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; DEFORMATION; FINITE VOLUME METHOD; ITERATIVE METHODS; MESH GENERATION; OSCILLATING CYLINDERS; OSCILLATING FLOW; TRANSONIC AERODYNAMICS; TWO PHASE FLOW;

COMPUTATIONAL RESULTS; FLOW INDUCED VIBRATIONS; FLUID STRUCTURAL INTERACTIONS; GAUSS SEIDEL ITERATION; LIMIT CYCLE OSCILLATION (LCO); NUMERICAL METHODOLOGIES; STEADY-STATE FLOW CONDITIONS; SUCCESSIVE ITERATION;

NAVIER STOKES EQUATIONS;

EID: 85088720857     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-2240     Document Type: Conference Paper

References (31)

1. R. B. Melville and S. A. Morton, "Fully Implicit Aeroelasticity on Oveerset Grid Systems. AIAA Paper-98-0521, 1998.
2. O. Bendiksen and K. Kousen, "Transonic Flutter Analysis Using the Euler Equations. AIAA Paper 87-0911, 1987.
3. G. Guruswamy, "Unsteady Aerodynamic and Aeroelastic Calculations for Wngs Using Euler Equations, AIAA Journal, vol. 28, pp. 461-469, March 1990.
4. E. Lee-Rausch and J. Batina, "Wing Flutter Computations Using an Aerodynamics Model Based on the Navier-Stokes Equations, Journal of Aircraft, vol. 33, pp. 1139-1147.
5. M. Smith, "Flight Loads Prediction Methods for Aircraft: Vol I. Euler/Navier-Stokes Aeroelas- tic Method (ENS3DAE) Technical Development Summary: Version 4.0. WRDC-TR-89-3104, 1989.
6. S. Vermeersch, P. Raj, R. Weed, and L. Sankar, "Towards Cost-Effective Aeroelastic Analysis on Advanced Parallel Computing Systems. AIAA Paper 97-0646, 1997.
7. S. Darracq, S. Champagneux, and A. Corjon, "Computation of Unsteady Turbulent Airfoil Flows with an Aeroelastic AUSM+ Implicit Solver. AIAA Paper-98-2411, 1998.
8. B. B. Prananta, H. M. H. L., and Z. R. J., "Two-Dimensional Transonic Aeroelastic Analysis Using Thin-Layer Navier-Stokes Method, Journal of Fluid and Structures, vol. 12, pp. 655- 676, 1998.
9. J. Bohbot and D. Darracq, Time Domain Analysis of Two D.O.F. Airfoil Flutter Using an Euler/Turbulent Navier-Stokes Implicit Solver. International Forum on Aeroelasticity and Structural Dynamics, Madrid, Spain, June 5-7, 2001.
10. F. J. Blom and P. Leyland, "Analysis of Fluid-Structure Interaction by Means of Dynamic Unstructured Meshes. AD-Vol. 53-3, 4th International Symposium on Fluid-Structure Inter- action, Aeroelasticity, Flow-Induced Vibrations and Noise, Volume I, ASME, 1997.
11. J. J. Alonso and A. Jameson, "Fully-Implicit Time-Marching Aeroelastic Solutions. AIAA Paper 94-0056, 1994.
12. J. Alonso, L. Martinelli, and A. Jameson, "Multigrid Unsteady Navier-Stokes Calculations with Aeroelastic Applications. AIAA Paper 95-0048, 1995.
13. S. A. Morton, R. B. Melville, and M. R. Visbal, "Accuracy and Coupling Issues of Aeroelastic Navier-Stokes Solutions on Deforming Meshes. AIAA Paper-97-1085, 1997.
14. R. B. Melville, S. A. Morton, and D. P. Rizzetta, "Implementation of a Fully-Implicit, Aeroe- lastic Navier-Stokes Solver. AIAA Paper-97-2039, 1997.
15. F. Liu, J. Cai, Y. Zhu, A. Wong, and H. Tsai, "Calculation of Wing Flutter by a Coupled CFD-CSD Method. AIAA-2000-0907, 2000.
16. S. Yoon and A. Jameson, "An LU-SSOR Scheme for the Euler and Navier-Stokes Equations. AIAA Paper 87-600, 1987.
17. G.-C. Zha and Z.-J. Hu, "Calculation of Transonic Internal Flows Using an E±cient High Resolution Upwind Scheme, AIAA Journal, Feb. 2004.
18. B. Baldwin and H. Lomax, "Thin-Layer Approximation and Algebraic Model for Separated Turbulent flows. AIAA Paper 78-257, 1978.
19. A. Jameson, "Time Dependent Calculations Using Multigrid with Application to Unsteady Flows past Airfoils and Wings. AIAA Paper 91-1596, 1991.
20. P. Roe, "Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes, Journal of Computational Physics, vol. 43, pp. 357-372, 1981.
21. B. Van Leer, "Towards the Ultimate Conservative Difference Scheme, III, Journal of Com- putational Physics, vol. 23, pp. 263-75, 1977.
22. P. Thomas and C. Lombard, "Geometric Conservation Law and Its Application to Flow Com- putations on Moving Grids, AIAA Journal, vol. 17, pp. 1030-1037.
23. A. Roshko, "On the Development of TurbulentWakes From Vortex Streets. NACA Rep. 1191, 1954.
24. S. Goldstein, "Modern Developments in Fluid Dynamics. Clarendon Press, Oxford, 1938.
25. O. Griffn, "Vortex-Induced Vibrations of Marine Structures in Uniform and Sheared Cur- rents. NSF Workshop on Riser Dynamics, Uiversity of Michigan, 1992.
26. H. Blackburn and G. Karniadakis, "Two and Three-Dimensional Vortex-Induced Vibration of a Circular Cylinder. ISOPE-93 Conference, Singapore, 1993.
27. P. Cook, M. McDonald, and M. Firmin, "Aerofoil rae 2822 - pressure distributions, and bound- ary layer and wake measurements. experimental data base for computer program assessment, Tech. Rep. AGARD Report AR-138, AGARD, 1979.
28. S. S. Davis, "NACA 64 A010 (NACA Ames Model) Oscillatory Pitching, Tech. Rep. AGARD Report No. 702, AGARD, August 1982.
29. M. McMullen, A. Jameson, and J. Alonso, "Application of a Non-Linear Frequency Domain Solver to the Euler and Navier-Stokes Equations. AIAA Paper-2002-0120, 2002.
30. K. Isogai, "Transonic Dip Mechanism of Flutter of a Sweptback Wing: Part II, AIAA Journal, vol. 19, pp. 1240-1242, September 1981.
31. K. Kousen and O. Bendiksen, "Nonlinear Aspects of the Transonic Aeroelastic Stability Prob- lem. AIAA Paper 88-2306, 1988.