Accurate numerical simulation of compressible transitional flows in turbomachinery

AIAA Journal

Volumn 40, Issue 4, 2002, Pages 702-708

  De Palma, P ^a  

^a POLITECNICO DI BARI   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMPUTER SIMULATION; EXTRAPOLATION; FINITE VOLUME METHOD; FLOW PATTERNS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; RUNGE KUTTA METHODS; TRANSITION FLOW; TURBINES; TURBULENCE; VORTEX SHEDDING;

COMPRESSIBLE TRANSITIONAL FLOWS;

COMPRESSIBLE FLOW;

EID: 0036530735     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1702     Document Type: Article

References (19)

1. The role of laminar-turbulent transition in gas turbine engines
2. Accurate and efficient solutions of unsteady viscous flows
3. Numerical simulation of transitional turbomachinery flows
4. On explicit algebraic stress models for complex turbulent flows
5. The effect of vortex shedding on the unsteady pressure distribution around the trailing edge of a turbine blade
6. Influence of free-stream turbulence and blade pressure gradient on boundary layer and loss behavior of turbine cascades
7. Assessment of two-equation turbulence models for transonic flows
8. Progress in the development of a Reynolds stress turbulence closure
9. Prediction of nonequilibrium turbulent flows with explicit algebraic stress models
10. Some properties of boundary layer flow during transition from laminar to turbulent motion
11. Approximate riemann solvers, parameter vectors and difference schemes
12. Intergration of navier-stokes equations using dual time stepping and a multigrid method
13. Validation of a multigrid method for the reynolds averaged equations
14. Guide to multigrid development
15. Time-dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
16. Vortex shedding behind a blunt trailing edge blade
17. A numerical study of the influence of grid refinement and turbulence modeling on the flow field inside a highly loaded turbine cascade
18. Test case E/CA-6 subsonic turbine cascade T106