-
1
-
-
0039371684
-
Filtering algebraic turbulence models for supersonic high-incidence missile flows
-
Sorrento, Italy
-
M. Amato, G. Iaccarino, Filtering algebraic turbulence models for supersonic high-incidence missile flows, in: RTO AVT Symp. on Missile Aerodynamics, Sorrento, Italy, 1998.
-
(1998)
RTO AVT Symp. on Missile Aerodynamics
-
-
Amato, M.1
Iaccarino, G.2
-
2
-
-
85035308704
-
Introduction to turbulence modeling for compressible flows
-
von Karman
-
B. Aupoix, Introduction to Turbulence Modeling for Compressible Flows, von Karman, Lecture Series, 2000.
-
(2000)
Lecture Series
-
-
Aupoix, B.1
-
3
-
-
0003262201
-
A one-equation turbulence transport model for high Reynolds number wall-bounded flows
-
B. Baldwin, T.J. Barth, A one-equation turbulence transport model for high Reynolds number wall-bounded flows, AIAA Paper 91-0610, 1991.
-
(1991)
AIAA Paper 91-0610
-
-
Baldwin, B.1
Barth, T.J.2
-
4
-
-
0004027614
-
Thin layer approximation of algebraic model for separated flows
-
B.S. Baldwin, H. Lomax, Thin layer approximation of algebraic model for separated flows, AIAA Paper 78-0257, 1978.
-
(1978)
AIAA Paper 78-0257
-
-
Baldwin, B.S.1
Lomax, H.2
-
6
-
-
0042908771
-
Numerical simulation of roll induced moment of cruciform tactical missiles
-
S. Ben Khelil, Ph. Guillen, M. Lazareff, R.G. Lacau, Numerical simulation of roll induced moment of cruciform tactical missiles, Aerospace Science and Technology 5 (2001) 109-124.
-
(2001)
Aerospace Science and Technology
, vol.5
, pp. 109-124
-
-
Ben Khelil, S.1
Guillen, Ph.2
Lazareff, M.3
Lacau, R.G.4
-
10
-
-
4244083554
-
Numerical simulation of side loads in an ideal truncated nozzle
-
to appear
-
S. Deck, Ph. Guillen, Numerical simulation of side loads in an ideal truncated nozzle, AIAA J. Propulsion Power, to appear.
-
AIAA J. Propulsion Power
-
-
Deck, S.1
Guillen, Ph.2
-
11
-
-
0039964030
-
Simulations numériques des écoulements décollés dans les tuyères
-
Arcachon, France
-
S. Deck, R. Hallard, Simulations numériques des écoulements décollés dans les tuyères, in: 37eme colloque d'Aérodynamique Appliquée, Aérodynamique et Propulsion des véhicules à grande vitesse, Arcachon, France, 2001, pp. 103-111.
-
(2001)
37eme Colloque d'Aérodynamique Appliquée, Aérodynamique et Propulsion des Véhicules à Grande Vitesse
, pp. 103-111
-
-
Deck, S.1
Hallard, R.2
-
12
-
-
0003255094
-
Computation of supersonic viscous flows around pointed bodies at large incidence
-
D. Degani, L.B. Schiff, Computation of supersonic viscous flows around pointed bodies at large incidence, AIAA Paper 83-0034, 1983.
-
(1983)
AIAA Paper 83-0034
-
-
Degani, D.1
Schiff, L.B.2
-
14
-
-
0040557061
-
Couche limite autour d'un fuselage en incidence en écoulement supersonique
-
Sorrento, Italy
-
P. d'Espiney, P. Champigny, D. Baudin, J.A. Pilon, Couche limite autour d'un fuselage en incidence en écoulement supersonique, in: RTO AVT Symp. on Missile Aerodynamics, Sorrento, Italy, 1998.
-
(1998)
RTO AVT Symp. on Missile Aerodynamics
-
-
D'Espiney, P.1
Champigny, P.2
Baudin, D.3
Pilon, J.A.4
-
15
-
-
0039964032
-
Inlet design for JAPHAR flight test vehicle
-
Bangalore, India
-
P. Duveau, H. Esch, K. Triesch, Inlet design for JAPHAR flight test vehicle, in: XV ISABE Congress, Bangalore, India, 2001.
-
(2001)
XV ISABE Congress
-
-
Duveau, P.1
Esch, H.2
Triesch, K.3
-
16
-
-
84983137860
-
Assesment of algebraic and one-equation turbulence models for transonic turbulent flow around a full aircraft configuration
-
C. Gacherieu, C. Weber, Assesment of algebraic and one-equation turbulence models for transonic turbulent flow around a full aircraft configuration, AIAA Paper 98-32457, 1998.
-
(1998)
AIAA Paper 98-32457
-
-
Gacherieu, C.1
Weber, C.2
-
17
-
-
0023378605
-
Young, Lower-upper implicit scheme with multiple grids for the Euler equations
-
A. Jameson, Young, Lower-upper implicit scheme with multiple grids for the Euler equations, AIAA J. 25 (7) (1987).
-
(1987)
AIAA J.
, vol.25
, Issue.7
-
-
Jameson, A.1
-
18
-
-
0015300220
-
The prediction of laminarization with a 2-equation model of turbulence
-
W.P. Jones, B.E. Launder, The prediction of laminarization with a 2-equation model of turbulence, Internat. J. Heat Mass Transfer 15 (1972).
-
(1972)
Internat. J. Heat Mass Transfer
, vol.15
-
-
Jones, W.P.1
Launder, B.E.2
-
19
-
-
22144498798
-
A joint ONERA-DLR research project on high speed airbreathing propulsion
-
Paper IS-093, Florence, Italy
-
P. Novelli, W. Koschel, A joint ONERA-DLR research project on high speed airbreathing propulsion, in: XIV ISABE Congress, Paper IS-093, Florence, Italy, 1999.
-
(1999)
XIV ISABE Congress
-
-
Novelli, P.1
Koschel, W.2
-
20
-
-
0026867287
-
Basic experiment on a supersonic vortex flow around a missile a missile body
-
D. Pagan, P. Molton, J. Delery, Basic experiment on a supersonic vortex flow around a missile a missile body, AIAA J. Spacecraft Rockets 29 (3) (1992) 373-378.
-
(1992)
AIAA J. Spacecraft Rockets
, vol.29
, Issue.3
, pp. 373-378
-
-
Pagan, D.1
Molton, P.2
Delery, J.3
-
22
-
-
0039371677
-
Algebraic turbulence modelling for vortical flows around slender bodies
-
Sorrento, Italy
-
N. Qin, C. Jayatunga, Algebraic turbulence modelling for vortical flows around slender bodies, in: RTO AVT Symp. on Missile Aerodynamics, Sorrento, Italy, 1998.
-
(1998)
RTO AVT Symp. on Missile Aerodynamics
-
-
Qin, N.1
Jayatunga, C.2
-
23
-
-
2942757053
-
Approximate Riemann solvers, parameter vectors and difference schemes
-
P.L. Roe, Approximate Riemann solvers, parameter vectors and difference schemes, J. Comput. Phys. 43 (1981).
-
(1981)
J. Comput. Phys.
, vol.43
-
-
Roe, P.L.1
-
24
-
-
0003058611
-
Advances in overset CFD processes applied to subsonic high-lift aircraft
-
S.E. Rogers, K. Both, S.M. Nash, M.D. Baker, J.P. Slotnick, M. Whitlock, H.V. Cao, Advances in overset CFD processes applied to subsonic high-lift aircraft, AIAA Paper 2000-4126, 1999.
-
(1999)
AIAA Paper 2000-4126
-
-
Rogers, S.E.1
Both, K.2
Nash, S.M.3
Baker, M.D.4
Slotnick, J.P.5
Whitlock, M.6
Cao, H.V.7
-
26
-
-
0027988926
-
A one equation turbulence model for aerodynamic flows
-
P.R. Spalart, S.R. Allmaras, A one equation turbulence model for aerodynamic flows, in: La Recherche Aérospatiale, 1994, pp. 5-21.
-
(1994)
La Recherche Aérospatiale
, pp. 5-21
-
-
Spalart, P.R.1
Allmaras, S.R.2
-
27
-
-
34249988639
-
Towards the ultimate conservative scheme II: Monotonicity and conservation combined in a second order scheme
-
B. Van Leer, Towards the ultimate conservative scheme II: Monotonicity and conservation combined in a second order scheme, J. Comput. Phys. 14 (1974).
-
(1974)
J. Comput. Phys.
, vol.14
-
-
Van Leer, B.1
|