-
1
-
-
33745535872
-
Accuracy of unstructured grid techniques workshop
-
Salas, M. D. (Ed.) January NASA Langley Research Centre, Hampton, Virginia (to be published)
-
Salas, M. D. (Ed.) Accuracy of unstructured grid techniques workshop. In NASA Proceedings, January 1990 (NASA Langley Research Centre, Hampton, Virginia) (to be published).
-
(1990)
NASA Proceedings
-
-
-
2
-
-
84985315986
-
Construction of curvilinear coordinate systems and applications of mesh generation
-
Gordon, W. J. and Hall, C. A. Construction of curvilinear coordinate systems and applications of mesh generation. Int. J. Numer. Meth. Engng, 1973, 7, 461-477.
-
(1973)
Int. J. Numer. Meth. Engng
, vol.7
, pp. 461-477
-
-
Gordon, W.J.1
Hall, C.A.2
-
3
-
-
17544392187
-
Generation of boundary-conforming grids around wing-body configurations using transfinite interpolation
-
Eriksson, L. E. Generation of boundary-conforming grids around wing-body configurations using transfinite interpolation. Am. Inst. Aeronaut. Astronaut. J., 1982, 20(10), 13131320.
-
(1982)
Am. Inst. Aeronaut. Astronaut. J.
, vol.20
, Issue.10
, pp. 13131320
-
-
Eriksson, L.E.1
-
4
-
-
2142708888
-
Solution of the 2-D unsteady Euler equations on a structured moving grid
-
University of Bristol
-
Williams, A. L. and Fiddcs, S. R Solution of the 2-D unsteady Euler equations on a structured moving grid. Department of Aerospace Engineering report 453, University of Bristol, 1992.
-
(1992)
Department of Aerospace Engineering Report 453
-
-
Williams, A.L.1
Fiddcs, S.R.2
-
5
-
-
0029255694
-
Central-difference and upwind-biased schemes for steady and unsteady Euler aerofoil computations
-
Alien, C. B. Central-difference and upwind-biased schemes for steady and unsteady Euler aerofoil computations. Aero. J., 1995, 99(982), 52-62.
-
(1995)
Aero. J.
, vol.99
, Issue.982
, pp. 52-62
-
-
Alien, C.B.1
-
6
-
-
0030736128
-
The reduction of numerical entropy generated by unsteady shockwaves
-
Alien, C. B. The reduction of numerical entropy generated by unsteady shockwaves. Aero. J., 1997, 101(1001), 7-16.
-
(1997)
Aero. J.
, vol.101
, Issue.1001
, pp. 7-16
-
-
Alien, C.B.1
-
8
-
-
0029138594
-
The development of a structured mesh grid adaptation technique for resolving shock discontinuities in upwind Navier-Stokes codes
-
Patel, M. K., Pericleous, K. A. and Baldwin, S. The development of a structured mesh grid adaptation technique for resolving shock discontinuities in upwind Navier-Stokes codes. Int. J. Numer. Meth. Fluids, 1995, 20.
-
(1995)
Int. J. Numer. Meth. Fluids
, pp. 20
-
-
Patel, M.K.1
Pericleous, K.A.2
Baldwin, S.3
-
10
-
-
33745560371
-
Unsteady compressible airfoil aerodynamics using an adaptive time-discontinuous GLS finite element method
-
Webster, B. E., Shephard, M. S., Rusak, Z. and Flaherty, J. E. Unsteady compressible airfoil aerodynamics using an adaptive time-discontinuous GLS finite element method. AIAA paper 93-0339, 1993.
-
(1993)
AIAA Paper 93-0339
-
-
Webster, B.E.1
Shephard, M.S.2
Rusak, Z.3
Flaherty, J.E.4
-
11
-
-
0020223604
-
Flux-vector splitting for the Euler equations
-
Van-Leer, B. Flux-vector splitting for the Euler equations. Lecture Notes in Physics, Vol. 170, 1982, pp. 507-512.
-
(1982)
Lecture Notes in Physics
, vol.170
, pp. 507-512
-
-
Van-Leer, B.1
-
12
-
-
0023834189
-
Van-Leer flux-vector splitting in moving coordinates
-
January
-
Parpia, I. H. Van-Leer flux-vector splitting in moving coordinates. Am. Inst. Aeronaut. Astronaut. J., January 1988, 26, 113-115.
-
(1988)
Am. Inst. Aeronaut. Astronaut. J.
, vol.26
, pp. 113-115
-
-
Parpia, I.H.1
-
13
-
-
0022783786
-
Comparison of finite volume flux vector splittings for the Euler equations
-
September
-
Anderson, W. K., Thomas, J. L. and Van-Leer, B. Comparison of finite volume flux vector splittings for the Euler equations. Am. Inst. Aeronaut. Astronaut. J., September 1986, 24, 1453-1460.
-
(1986)
Am. Inst. Aeronaut. Astronaut. J.
, vol.24
, pp. 1453-1460
-
-
Anderson, W.K.1
Thomas, J.L.2
Van-Leer, B.3
-
14
-
-
0002374896
-
Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings
-
Jameson, A. Time dependent calculations using multigrid, with applications to unsteady flows past airfoils and wings. AIAA paper 91-1596, 1991.
-
(1991)
AIAA Paper 91-1596
-
-
Jameson, A.1
-
15
-
-
0018529022
-
Geometrie conservation law and its application to flow computations on moving grids
-
October
-
Thomas, P. D. and Lombard, C. K. Geometrie conservation law and its application to flow computations on moving grids. Am. Inst. Aeronaut. Astronaut. J., October 1979, 17, 1030-1037.
-
(1979)
Am. Inst. Aeronaut. Astronaut. J.
, vol.17
, pp. 1030-1037
-
-
Thomas, P.D.1
Lombard, C.K.2
-
16
-
-
0345962617
-
Test cases for inviscid flow field methods
-
Anon. Test cases for inviscid flow field methods. AGARD Agardograph AR-211, 1985.
-
(1985)
AGARD Agardograph AR-211
-
-
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