Fully coupled fluid-structural interactions using an efficient high resolution upwind scheme

Journal of Fluids and Structures

Volumn 20, Issue 8, 2005, Pages 1105-1125

  Chen, X Y ^a   Zha, G C ^a  

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

Author keywords

Flow induced vibration; Fluid structural interaction; Flutter; Low diffusion upwind scheme

Indexed keywords

AIRFOILS; CALCULATIONS; COMPUTATIONAL FLUID DYNAMICS; DIFFUSION; ELASTICITY; FLOW OF FLUIDS; MATHEMATICAL TRANSFORMATIONS; MATRIX ALGEBRA; VECTORS; VIBRATIONS (MECHANICAL);

FLOW INDUCED VIBRATION; FLUTTER; HIGH RESOLUTION UPWIND SCHEME; LOW DIFFUSION UPWIND SCHEME;

FLUID STRUCTURE INTERACTION;

AEROFOIL; FLOW INDUCED VIBRATION; FLUID-STRUCTURE INTERACTION; FLUTTER;

EID: 23844541284     PISSN: 08899746     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2005.02.011     Document Type: Article

References (37)

1. Alonso J.J. Jameson A. 1994 Fully-implicit time-marching aeroelastic solutions. AIAA Paper 94-0056.
2. Alonso J.J. Martinelli L. Jameson A. 1995 Multigrid unsteady Navier-Stokes calculations with aeroelastic applications. AIAA Paper 95-0048.
3. Baldwin B.S. Lomax H. 1978 Thin-layer approximation and algebraic model for separated turbulent flows. AIAA Paper 78-257.
4. Bendiksen O.O. Kousen K.A. 1987 Transonic flutter analysis using the Euler equations. AIAA Paper 87-0911.
5. Blackburn H.M. Karniadakis G.E. 1993 Two and three-dimensional vortex-induced vibration of a circular cylinder. ISOPE-93 Conference, Singapore.
6. Blom F.J. Leyland P. 1997 Analysis of fluid-structure interaction by means of dynamic unstructured meshes. AD-Vol. 53-3 Fourth International Symposium on Fluid-Structure Interaction Aeroelasticity Flow-Induced Vibrations and Noise vol. I ASME.
7. Bohbot J. Darracq D. 2001 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.
8. Chen X.-Y. Zha G.-C. Hu Z.-J. 2004 Numerical simulation of flow induced vibration based on fully coupled-structural interactions. AIAA Paper 2004-2240.
9. Cook P.H. McDonald M.A. Firmin M.C.P. 1979 Aerofoil RAE 2822-Pressure distributions, and boundary layer and wake measurements. Experimental data base for computer program assessment. AGARD Report AR-138.
10. Darracq S. Champagneux S. Corjon A. 1998 Computation of unsteady turbulent airfoil flows with an aeroelastic AUSM+ implicit solver. AIAA Paper 98-2411.
11. Davis S.S. 1982 NACA 64 A010 (NACA Ames model) oscillatory pitching AGARD Report No. 702.
12. Edwards J.R. 1995 A low-diffusion flux-splitting scheme for Navier-Stokes calculations. AIAA Paper 95-1703-CP.
13. J.R. Edwards A low-diffusion flux-splitting scheme for Navier-Stokes calculations Computer & Fluids 6 1997 635-659
14. Giles M.B. 1995 Stability and accuracy of numerical boundary conditions in aeroelastic analysis. Report No. 95/13 Oxford University Computing Laboratory.
15. S. Goldstein Modern Developments in Fluid Dynamics 1938 Clarendon Press Oxford
16. Griffin O.M. 1992 Vortex-induced vibrations of marine structures in uniform and sheared currents. NSF Workshop on Riser Dynamics University of Michigan.
17. G.P. Guruswamy Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations AIAA Journal 28 1990 461-469
18. Hänel, D. Schwane R. Seider G. 1987 On the accuracy of upwind schemes for the solution of the Navier-Stokes eqautions AIAA paper 87-1105-CP.
19. K. Isogai Transonic dip mechanism of flutter of a sweptback wing part II AIAA Journal 19 1981 1240-1242
20. Jameson A. 1991 Time dependent calculations using multigrid with application to unsteady flows past airfoils and wings. AIAA Paper 91-1596.
21. Jameson A. 1993 Analysis and design of numerical schemes for gas dynamics I: Artificial diffusion, upwind biasing, limiters and their effect on accuracy and multigrid convergence in transonic and hypersonic flow. AIAA Paper 93-3359.
22. A. Jameson Analysis and design of numerical schemes for gas dynamics I: Artificial diffusion, upwind biasing, limiters and their effect on accuracy and multigrid convergence in transonic and hypersonic flow Journal of Computational Fluid Dynamics 4 1995 171-218
23. A. Jameson Analysis and design of numerical schemes for gas dynamics II: artificial diffusion and discrete shock structure Journal of Computational Fluid Dynamics 5 1995 1-38
24. E.M. Lee-Rausch J.T. Batina Wing flutter computations using an aerodynamics model based on the Navier-Stokes equations Journal of Aircraft 33 1996 1139-1147
25. +. Journal of Computational Physics 129 1996 364-382
26. Liu F. Cai J. Zhu Y. Wong A.S.F. Tsai H.M. 2000 Calculation of wing flutter by a coupled CFD-CSD method. AIAA 2000-0907.
27. McMullen M. Jameson A. Alonso J. 2002 Application of a non-linear frequency domain solver to the Euler and Navier-Stokes equations. AIAA Paper 2002-0120.
28. Melville R.B. Morton S.A. 1998 Fully implicit aeroelasticity on overset grid systems. AIAA Paper 98-0521.
29. Melville R.B. Morton S.A. Rizzetta D.P. 1997 Implementation of a fully-implicit aeroelastic Navier-Stokes solver. AIAA Paper 97-2039.
30. Morton S.A. Melville R.B. Visbal M.R. 1997 Accuracy and coupling issues of aeroelastic Navier-Stokes solutions on deforming meshes. AIAA Paper 97-1085.
31. B.B. Prananta M.H.L. Hounjet R.J. Zwaan Two-dimensional transonic aeroelastic analysis using thin-layer Navier-Stokes method Journal of Fluid and Structures 12 1998 655-676
32. Roshko A. 1954 On the development of turbulent wakes from vortex streets. NACA Report No. 1191.
33. Smith M.J. 1989 Flight loads prediction methods for aircraft: Vol. I. Euler/Navier-Stokes aeroelastic method (ENS3DAE) technical development summary: Version 4.0. WRDC-TR-89-3104.
34. P.D. Thomas C.K. Lombard Geometric conservation law and its application to flow computations on moving grids AIAA Journal 17 1979 1030-1037
35. Vermeersch S.A. Raj P. Weed R.A. Sankar L.N. 1997 Towards cost-effective aeroelastic analysis on advanced parallel computing systems. AIAA Paper 97-0646.
36. Zha G.-C. 2004 A low diffusion E-CUSP upwind scheme for transonic flows. AIAA Paper 2004-2707.
37. G.-C. Zha Z.-J. Hu Calculation of transonic internal flows using an efficient high resolution upwind scheme AIAA Journal 42 2004 205-214