A zonal method for unsteady, viscous, compressible airfoil flows

Journal of Fluids and Structures

Volumn 8, Issue 1, 1994, Pages 107-123

  Ekaterinaris, J A ^a   Cricelli, A S ^b   Platzer, M F ^b  

^a NASA AMES RESEARCH CENTER   (United States)

^b NAVAL POSTGRADUATE SCHOOL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROFOILS; MODELLING-MATHEMATICAL; SEPARATED; VISCOUS FLOW; ZONAL;

EID: 0028039331     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1006/jfls.1994.1005     Document Type: Article

References (26)

1. Baldwin, B. S. & Lomax, H. 1978 Thin layer approximation and algebraic model for separated turbulent flows. AIAA Paper 78-257.
2. Benek, J. A., Bunning, P. G. & Steger, J. L. 1985 A 3D Chimera grid embedding technique. AIAA Paper 85-1523.
3. Chakravarthy, S. R. & Osher, S. 1985 A new class of high accuracy TVD schemes for hyperbolic conservation laws. AIAA Paper 85-0363.
4. Chandrasekhara, M., Ahmed, S. & Carr, L. 1990 Schlieren studies of compressibility effects on dynamic stall of airfoils in transient pitching motion. AIAA Paper-90-3038.
5. Chesshjre, G. & Henshaw, W. D. 1990 Composite overlapping meshes for solution of partial differential equations. Journal of Computational Physics 90, 1-64.
6. Clarkson, J. D., Ekaterinaris, J. A. & Platzer, M. F. 1993 Computational investigation of airfoil stall flutter. In Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines and Propellers (ed. H. M. Atassi), pp. 415-432. Springer-Verlag.
7. Ekaterinaris, J. A. 1089 Compressible Studies on Dynamic Stall. AIAA Paper 89-0024.
8. Harris, C. D. 1981 Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8 foot transonic pressure tunnel. NASA TM 81927.
9. Hirsch, C. 1990 Numerical Computation of Internal and External Flows New York: Wiley.
10. Hanel, D. 1992 Computational techniques for solving the Navier-Stokes equations. AGARD- CP-510, Paper No. 1.
11. Jang, H. M., Ekaterinaris, J. A., Platzer, M. F., & Cebeci, T. 1991 Essential ingredients for the computation of steady and unsteady boundary layers. Journal of Turbomachinery 13, 608-616.
12. Johnson, D. A. & King, L. S. 1985 A mathematically simple turbulence closure model for attached and separated turbulent boundary layers. AIAA Journal 23, 1864-1692.
13. Landon, R. H. 1982 NACA 0012 Oscillatory and transient pitching. AGARD-R-702.
14. Osher, S. & Solomon, F. 1982 Upwind difference schemes for hyperbolic systems of conservation laws. Mathematics of Computation 38, 339-374.
15. Osher, S. & Chakravarthy, S. R. 1983 Upwind schemes and boundary conditions with applications to Euler equations in general geometries Journal of Computational Physics 50, 447-481.
16. Rai, M. M. 1986 A relaxation approach to patched-grid calculations with the Euler equations. Journal of Computational Physics 66, 99-131.
17. Rai, M. M. 1987a Navier-Stokes simulations of rotor-stator interaction using patched and overlaid grids. AIAA Journal of Propulsion and Power 3, 387-396.
18. Rai, M. M. 1987b Unsteady three-dimensional Navier-Stokes simulations of turbine rotor-stator interaction. AIAA Paper 87-2085.
19. Rai, M. M. & Chakravarthy, S. R. 1986 An implicit form of the Osher upwind scheme. AIAA Journal 24, 735-743.
20. Roe, P. 1985 Some contributions to the modeling of discontinuous flows. Large Scale Computations in Fluid Mechanics. Lectures in Applied Mathematics, American Mathematical Society, Vol. 22, pp. 161-193.
21. Rumsey, C. L. & Anderson, W. K. 1988 Some numerical and physical aspects of unsteady Navier-Stokes computations over airfoils using dynamic meshes. AIAA Paper 88-0329.
22. Steger, J. L. & Warming, R. F. 1981 Flux vector splitting of the inviscid gas dynamic equations with applications to finite-difference methods. Journal of Computational Physics 40, 263-293.
23. Visbal, M. R. 1988 Effect of compressibility on dynamic stall of a pitching airfoil. AIAA Paper 88-0132.
24. Yakhot, V., Orszag, S. A. 1986 Renormalization group analysis of turbulence. I. Basic theory. Journal of Scientific Computing 1, 1-31.
25. Yee, H. C., Warming, R. F. & Harden, A. 1983 Implicit total variation diminishing (TVD) schemes for steady-state calculations. NASA TM-84323.
26. Yee, H. C., 1989 A class of high-resolution explicit and implicit shock-capturing methods. NASA-TM 101088.