Large-eddy simulation of supersonic compression-ramp flow by high-order method

AIAA Journal

Volumn 39, Issue 12, 2001, Pages 2283-2292

  Rizzetta, D P ^a   Visbal, M R ^a   Gaitonde, D V ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; APPROXIMATION THEORY; COMPUTER SIMULATION; FINITE DIFFERENCE METHOD; MATHEMATICAL MODELS; SHOCK WAVES;

SPATIAL FILTERS;

SUPERSONIC FLOW;

EID: 0035659424     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1266     Document Type: Article

References (50)

1. Consistent initial conditions for the DNS of compressible turbulence
2. Direct simulation of spatially evolving compressible turbulent boundary layers
3. Large-eddy simulation of a spatially evolving supersonic turbulent boundary-layer flow
4. A dynamic subgrid-scale eddy viscosity model
5. Direct numerical simulation of isotropic turbulence interacting with a weak shock wave
6. Large-eddy simulation of the shock/turbulence interaction
7. Some new aspects of the shockwave/boundary-layer interaction in compression-ramp flows
8. Experimental study of three shock wave/turbulent boundary layer interactions
9. Unsteadiness of the separation shock wave structure in a supersonic compression ramp flowfield
10. Unsteadiness of the shock wave structure in attached and separated compression ramp flows
11. Unsteady wave structure near separation in a mach 5 compression ramp interaction
12. Correlation of separation shock motion with pressure fluctuations in the incoming boundary layer
13. Detailed Study of attached and separated compression corner flowfields in high reynolds number supersonic flow
14. A very large-eddy simulation of an unsteady shock-wave/turbulent boundary-layer interaction
15. Compressible large-eddy simulation using unstructured grid: Supersonic turbulent boundary layer and compression corner
16. Large-eddy simulation of a supersonic compression corner Part I
17. Direct numerical simulation of turbulent compression ramp flow
18. θ = 1685
19. Application of a high-order compact difference scheme to large-eddy and direct numerical simulation
20. General circulation experiments with the primitive equations
21. Statistical theory for compressible turbulent shear flows, with the application to subgrid modeling
22. A dynamic subgrid-scale model for compressible turbulence and scalar transport
23. A proposed modification of the germano subgrid-scale closure method
24. An implicit factored scheme for the compressible navier-stokes equations
25. Numerical simulation of delta-wing roll
26. Numerical solutions of the euler equations by finite volume methods using runge-kutta time stepping schemes
27. A diagonal form of an implicit approximate-factorization algorithm
28. High-order-accurate methods for complex unsteady subsonic flows
29. Direct numerical simulation of a forced transitional plane wall jet
30. Compact finite difference schemes with spectral-like resolution
31. Practical aspects of high-order accurate finite-volume schemes for electromagnetics
32. Approximate riemann solvers, parameter vectors and difference schemes
33. Flux-vector splitting for the euler equations
34. Towards the ultimate conservation difference scheme. V. A second-order sequel to Godunov's method
35. On central-differencing and upwind schemes
36. Numerical simulation of delta-wing roll
37. Computation of delta-wing roll maneuvers
38. Computational study of vortex breakdown on a pitching delta wing
39. Onset of vortex breakdown above a pitching delta wing
40. Numerical investigation of synthetic-jet flowfields
41. New insights into large eddy simulation
42. Monotonically integrated large-eddy simulation
43. An evaluation of theories for predicting skin friction and heat transfer on flat plates at supersonic and hypersonic mach numbers
44. On the turbulent flow near a wall
45. Mathematical and physical constraints on large-eddy simulation of turbulence
46. Direct numerical and large-eddy simulation of supersonic flows by a high-order method