The reduction of numerical entropy generated by unsteady shockwaves

Aeronautical Journal

Volumn 101, Issue 1001, 1997, Pages 9-16

  Allen, C B ^a  

^a UNIVERSITY OF BRISTOL   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; CALCULATIONS; DUCTS; ERRORS; FLUID DYNAMICS; NUMERICAL METHODS; OSCILLATIONS; PRESSURE;

EULER FLOWS; NUMERICAL ENTROPY; PRESSURE WAVES; SPURIOUS ENTROPY; UNSTEADY SHOCKWAVES;

SHOCK WAVES;

EID: 0030736128     PISSN: 00019240     EISSN: None     Source Type: Trade Journal    
DOI: None     Document Type: Article

References (16)

1. WOODWARD, P. and COLLELA, P. The numerical simulation of two-dimensional fluid flow through shocks, J Comp Phys, 54, (1), 1984, pp 115-173.
2. ROBERTS, T.W. The behaviour of flux-difference splitting schemes near slowly moving shockwaves, J Comp Phys, 90, (1), 1990, pp 141-160.
3. LINDQUIST, D.R. and GILES, M.B. On the validity of linearized unsteady Euler equations with shock capturing, AIAA Paper 91-1598, June 1991.
4. MEADOWS, K.R., CAUGHEY, D.A. and CASPER, J. Computing unsteady shockwaves for aeroacoustic applications, AIAA J, 32, (7), 1994, pp 1360-1366.
5. VAN-LEER, B. Flux-vector splitting for the Euler equations, Lecture Notes in Physics, 170, 1982, pp 507-512.
6. JAMESON, A. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings, AIAA Paper 91-1596, June 1991.
7. ANDERSON, W.K., THOMAS, J.L. and VAN-LEER, B. Comparison of finite volume flux vector splittings for the Euler equations, AIAA J, September 1986, 24, pp 1453-1460.
8. JAMESON, A., SCHMIDT, W. and TURKEL, E. Numerical solution of the Euler equations by finite-volume methods using Runge-Kutta time-stepping schemes, AIAA Paper 81-1259, 1981.
9. TURKEL, E. and VAN-LEER, B. Runge-Kutta Methods for Partial Differential Equations, ICASE Report, 1983.
10. PIKE, J. Exact Analytic Solutions for Viscous Shock-Waves with Implications for numerically Captured Shock-Waves, RAE Technical Report 85041, 1985.
11. PARPIA, I.H. Van-Leer flux-vector splitting in moving coordinates, AIAA J, January 1988, 26, pp 113-115.
12. THOMAS, P.D. and LOMBARD, C.K. Geometric Conservation Law and its application to flow computations on moving grids AIAA J, October 1979, 17, pp 1030-1037.
13. GORDON, W.J. and HALL, C.A. Construction of curvilinear coordinate systems and applications of mesh generation, Int J Num Methods Eng, 1973, 7, pp 461-477.
14. ERIKSSON, L.E. Generation of boundary-conforming grids around wingbody configurations using transfinite interpolation, AIAA J, 1982, 20, (10), pp 1313-1320.
15. ALLEN, C.B. Central-difference and upwind-biased schemes for steady and unsteady Euler aerofoil computations, Aeronaut J, 1995, 99, (982), pp 52-62.
16. (Anonymous) Compendium of unsteady aerodynamic measurements, AGARD-R-702, 1982.