-
1
-
-
0019042663
-
Vortex development on slender misiles at supersonic speeds
-
Allen J.M., Dillenius M.F.E., Vortex development on slender misiles at supersonic speeds, J. Spacecraft Rockets 17 (4) (1980) 377-378.
-
(1980)
J. Spacecraft Rockets
, vol.17
, Issue.4
, pp. 377-378
-
-
Allen, J.M.1
Dillenius, M.F.E.2
-
4
-
-
0022028484
-
Implicit upwind methods for the compressible Navier-Stokes equations
-
Coakley T.J., Implicit upwind methods for the compressible Navier-Stokes equations, AIAA J. 23 (3) (1983) 374-380.
-
(1983)
AIAA J.
, vol.23
, Issue.3
, pp. 374-380
-
-
Coakley, T.J.1
-
6
-
-
85031465340
-
Couche limite autour d'un fuselage de missile en incidence en écoulement supersonique
-
RTO-MP-5, AC/323(AVT)TP/3, Missiles Aerodynamics
-
d'Espiney P., Champigny P., Baudin D., Pilon J.A., Couche limite autour d'un fuselage de missile en incidence en écoulement supersonique. Etude expérimentale et calculs Navier-Stokes, RTO-MP-5, AC/323(AVT)TP/3, Missiles Aerodynamics (1998) 19.
-
(1998)
Etude Expérimentale et Calculs Navier-Stokes
, pp. 19
-
-
D'Espiney, P.1
Champigny, P.2
Baudin, D.3
Pilon, J.A.4
-
7
-
-
40749159424
-
High resolution schemes for hyperbolic conservation laws
-
Harten A., High resolution schemes for hyperbolic conservation laws, J. Comput. Phys. 49 (1983) 357-393.
-
(1983)
J. Comput. Phys.
, vol.49
, pp. 357-393
-
-
Harten, A.1
-
8
-
-
2442433925
-
Towards the ultimate conservative difference scheme V. A second order sequel to Godunov's methods
-
van Leer B., Towards the ultimate conservative difference scheme V. A second order sequel to Godunov's methods, J. Comput. Phys. 32 (1979) 101-136.
-
(1979)
J. Comput. Phys.
, vol.32
, pp. 101-136
-
-
Van Leer, B.1
-
9
-
-
0020223604
-
A flux vector splitting for the euler equations
-
van Leer B., A flux vector splitting for the Euler equations, Lecture Notes in Physics 170 (1982) 405-512.
-
(1982)
Lecture Notes in Physics
, vol.170
, pp. 405-512
-
-
Van Leer, B.1
-
11
-
-
0348196997
-
MESH3D : Un outil pour la construction de maillages tridimensionnels
-
CEL Biscarosse (France), ONERA TP 1992/164
-
Montigny-Rannou F., Jacquotte O.P., MESH3D : un outil pour la construction de maillages tridimensionnels, AAAF-29 ème colloque d'Aérodynamique Appliquée, CEL Biscarosse (France), ONERA TP 1992/164, 1992.
-
(1992)
AAAF-29 Ème Colloque d'Aérodynamique Appliquée
-
-
Montigny-Rannou, F.1
Jacquotte, O.P.2
-
12
-
-
0042920184
-
-
RTO-MP-5, AC/323(AVT)TP/3, Missiles Aerodynamics
-
Oktay E., Alemdaroǧlu N., Tarhan E., Champigny P., d'Espiney P., 3D Euler and thin layer Navier-Stokes solutions for missiles at supersonic speeds and high angles of attack, RTO-MP-5, AC/323(AVT)TP/3, Missiles Aerodynamics (1998) 27.
-
(1998)
3D Euler and Thin Layer Navier-Stokes Solutions for Missiles at Supersonic Speeds and High Angles of Attack
, pp. 27
-
-
Oktay, E.1
Alemdaroǧlu, N.2
Tarhan, E.3
Champigny, P.4
D'Espiney, P.5
-
13
-
-
2942757053
-
Approximation Riemann solvers. Parameter vector and difference schemes
-
Roe P.L., Approximation Riemann solvers. Parameter vector and difference schemes, J. Comput. Phys. 43 (1987) 357-372.
-
(1987)
J. Comput. Phys.
, vol.43
, pp. 357-372
-
-
Roe, P.L.1
-
14
-
-
46149152488
-
-
RTO-MP-5, AC/323(AVT)TP/3, Missiles Aerodynamics
-
Srivastava B., Furtek J., Shelton A., Paduano R., Role of CFD in missile aerodynamic design: A review of recent efforts at raytheon, RTO-MP-5, AC/323(AVT)TP/3, Missiles Aerodynamics (1998) 33.
-
(1998)
Role of CFD in Missile Aerodynamic Design: A Review of Recent Efforts at Raytheon
, pp. 33
-
-
Srivastava, B.1
Furtek, J.2
Shelton, A.3
Paduano, R.4
|