-
1
-
-
0033873396
-
Laminar-turbulent transition prediction in three-dimensional flows
-
Arnal D., and Casalis G. Laminar-turbulent transition prediction in three-dimensional flows. Progress in Aerospace Sciences 36 (2000) 173-191
-
(2000)
Progress in Aerospace Sciences
, vol.36
, pp. 173-191
-
-
Arnal, D.1
Casalis, G.2
-
2
-
-
55049111606
-
-
B.S. Baldwin, H. Lomax, Thin-layer approximation and algebraic model for separated turbulent flows, AIAA Paper 78-257, 1978
-
B.S. Baldwin, H. Lomax, Thin-layer approximation and algebraic model for separated turbulent flows, AIAA Paper 78-257, 1978
-
-
-
-
3
-
-
55049083545
-
-
G. Casalis, D. Arnal, ELFIN II Subtask 2.3: Database method - Development and validation of the simplified method for pure crossflow instability at low speed, ELFIN II - European Laminar Flow Investigation, Technical Report no 145, ONERA-CERT, Département d'Études et de Recherches en Aérothermodynamique (DERAT), R.T. DERAT no 119/5618.16, December 1996
-
G. Casalis, D. Arnal, ELFIN II Subtask 2.3: Database method - Development and validation of the simplified method for pure crossflow instability at low speed, ELFIN II - European Laminar Flow Investigation, Technical Report no 145, ONERA-CERT, Département d'Études et de Recherches en Aérothermodynamique (DERAT), R.T. DERAT no 119/5618.16, December 1996
-
-
-
-
4
-
-
0036684209
-
Transition prediction for three-dimensional boundary layers in computational fluid dynamics applications
-
Crouch J.D., Crouch I.W.M., and Ng L.L. Transition prediction for three-dimensional boundary layers in computational fluid dynamics applications. AIAA Journal 40 8 (2002) 1536-1541
-
(2002)
AIAA Journal
, vol.40
, Issue.8
, pp. 1536-1541
-
-
Crouch, J.D.1
Crouch, I.W.M.2
Ng, L.L.3
-
5
-
-
55049104931
-
-
R.M. Czerwiec, J.R. Edwards, C.L. Rumsey, A. Bertelrud, H.A. Hassan, Study of high-lift configurations using k - ζ transition/turbulence model, AIAA Paper 99-3186, 1999
-
R.M. Czerwiec, J.R. Edwards, C.L. Rumsey, A. Bertelrud, H.A. Hassan, Study of high-lift configurations using k - ζ transition/turbulence model, AIAA Paper 99-3186, 1999
-
-
-
-
6
-
-
0035447452
-
Development of a one-equation transition/turbulence model
-
Edwards J.R., Roy C.J., Blottner F.G., and Hassan H.A. Development of a one-equation transition/turbulence model. AIAA Journal 39 9 (2001) 1691-1698
-
(2001)
AIAA Journal
, vol.39
, Issue.9
, pp. 1691-1698
-
-
Edwards, J.R.1
Roy, C.J.2
Blottner, F.G.3
Hassan, H.A.4
-
7
-
-
55049105533
-
-
EUROLIFT II-European High Lift Programme II, Annex B: "Description of Work", A Specific Targeted Research Project of the 6th European Framework Program, GRD-2004-502896, 2004
-
EUROLIFT II-European High Lift Programme II, Annex B: "Description of Work", A Specific Targeted Research Project of the 6th European Framework Program, GRD-2004-502896, 2004
-
-
-
-
8
-
-
55049090044
-
-
FLOWer, Installation and User Handbook, Release 116, Doc. Nr. MEGAFLOW-1001, Institut für Entwurfsaerodynamik, Deutsches Zentrum für Luft- und Raumfahrt e.V., 2000
-
FLOWer, Installation and User Handbook, Release 116, Doc. Nr. MEGAFLOW-1001, Institut für Entwurfsaerodynamik, Deutsches Zentrum für Luft- und Raumfahrt e.V., 2000
-
-
-
-
9
-
-
0029406661
-
Computation of compressible, laminar boundary layers on swept, tapered wings
-
Horton H.P., and Stock H.W. Computation of compressible, laminar boundary layers on swept, tapered wings. Journal of Aircraft 32 (1995) 1402-1405
-
(1995)
Journal of Aircraft
, vol.32
, pp. 1402-1405
-
-
Horton, H.P.1
Stock, H.W.2
-
10
-
-
0042494161
-
N-database method for laminar-turbulent transition prediction on airfoils
-
New Results in Numerical and Experimental Fluid Mechanics III, Springer Verlag, Berlin, Heidelberg, New York
-
N-database method for laminar-turbulent transition prediction on airfoils. New Results in Numerical and Experimental Fluid Mechanics III. Notes on Numerical Fluid Mechanics vol. 77 (2002), Springer Verlag, Berlin, Heidelberg, New York 92-99
-
(2002)
Notes on Numerical Fluid Mechanics
, vol.77
, pp. 92-99
-
-
Krumbein, A.1
-
11
-
-
27144443110
-
Automatic transition prediction and application to high-lift multi-element configurations
-
also AIAA Paper 2004-2543, June/July 2004
-
Krumbein A. Automatic transition prediction and application to high-lift multi-element configurations. Journal of Aircraft 42 (2005) 1150-1164 also AIAA Paper 2004-2543, June/July 2004
-
(2005)
Journal of Aircraft
, vol.42
, pp. 1150-1164
-
-
Krumbein, A.1
-
12
-
-
33847744258
-
Automatic transition prediction and application to three-dimensional wing configurations
-
10.2514/1.22254 also AIAA Paper 2006-914, June 2006
-
Krumbein A. Automatic transition prediction and application to three-dimensional wing configurations. Journal of Aircraft 44 1 (2007) 119-133 10.2514/1.22254 also AIAA Paper 2006-914, June 2006
-
(2007)
Journal of Aircraft
, vol.44
, Issue.1
, pp. 119-133
-
-
Krumbein, A.1
-
13
-
-
54549093278
-
-
A. Krumbein, H.W. Stock, Laminar-turbulent transition modeling in Navier-Stokes solvers using engineering methods, in: ECCOMAS 2000, Barcelona (e), 11-14 September 2000, ECCOMAS 2000, CD-Rom Proceedings, editor: International Center for Numerical Methods in Engineering (CIMNE), 2000, ISBN: 84-89925-70-4, Depósito Legal: B-37139-2000
-
A. Krumbein, H.W. Stock, Laminar-turbulent transition modeling in Navier-Stokes solvers using engineering methods, in: ECCOMAS 2000, Barcelona (e), 11-14 September 2000, ECCOMAS 2000, CD-Rom Proceedings, editor: International Center for Numerical Methods in Engineering (CIMNE), 2000, ISBN: 84-89925-70-4, Depósito Legal: B-37139-2000
-
-
-
-
14
-
-
30744468823
-
-
R.B. Langtry, F.R. Menter, Transition modeling for general CFD applications in aeronautics, AIAA Paper 2004-522, 2005
-
R.B. Langtry, F.R. Menter, Transition modeling for general CFD applications in aeronautics, AIAA Paper 2004-522, 2005
-
-
-
-
15
-
-
55049141290
-
-
R. Radespiel, K. Graage, O. Brodersen, Transition predictions using Reynolds-averaged Navier-Stokes and linear stability analysis methods, AIAA Paper 91-1641, 1991
-
R. Radespiel, K. Graage, O. Brodersen, Transition predictions using Reynolds-averaged Navier-Stokes and linear stability analysis methods, AIAA Paper 91-1641, 1991
-
-
-
-
16
-
-
55049117928
-
-
R. Rudnik, A. Ronzheimer, M. Schenk, Berechnung von zwei- und dreidimensionalen Hochauftriebskonfigurationen durch Lösung der Navier-Stokes Gleichungen, in: Jahrbuch 1996, Bd. II der Deutschen Gesellschaft für Luft- und Raumfahrt, Lilienthal-Oberth e.V. (DGLR), JT 96-104, Deutscher Luft- und Raumfahrtkongreß, DGLR-Jahrestagung Sep. 1996, Dresden, Deutsche Gesellschaft für Luft- und Raumfahrt, Lilienthal-Oberth e.V. (DGLR), Godesberger Allee 70, D-53175 Bonn, Germany, 1996, pp. 717-726
-
R. Rudnik, A. Ronzheimer, M. Schenk, Berechnung von zwei- und dreidimensionalen Hochauftriebskonfigurationen durch Lösung der Navier-Stokes Gleichungen, in: Jahrbuch 1996, Bd. II der Deutschen Gesellschaft für Luft- und Raumfahrt, Lilienthal-Oberth e.V. (DGLR), JT 96-104, Deutscher Luft- und Raumfahrtkongreß, DGLR-Jahrestagung Sep. 1996, Dresden, Deutsche Gesellschaft für Luft- und Raumfahrt, Lilienthal-Oberth e.V. (DGLR), Godesberger Allee 70, D-53175 Bonn, Germany, 1996, pp. 717-726
-
-
-
-
17
-
-
84897585285
-
-
W.S. Saric, H.L. Reed, Toward practical laminar flow control - remaining challenges, AIAA Paper 2004-2311, June 2004
-
W.S. Saric, H.L. Reed, Toward practical laminar flow control - remaining challenges, AIAA Paper 2004-2311, June 2004
-
-
-
-
18
-
-
0038805681
-
Stability and transition of three-dimensional boundary layers
-
Saric W.S., Reed H.L., and White E.B. Stability and transition of three-dimensional boundary layers. Annu. Rev. Fluid. Mech. 35 (2003) 413-440
-
(2003)
Annu. Rev. Fluid. Mech.
, vol.35
, pp. 413-440
-
-
Saric, W.S.1
Reed, H.L.2
White, E.B.3
-
19
-
-
0024714069
-
Analysis of low Reynolds number separation bubbles using semi-empirical methods
-
Schmidt G.S., and Mueller J.Th. Analysis of low Reynolds number separation bubbles using semi-empirical methods. AIAA Journal 27 8 (1989) 993-1001
-
(1989)
AIAA Journal
, vol.27
, Issue.8
, pp. 993-1001
-
-
Schmidt, G.S.1
Mueller, J.Th.2
-
20
-
-
55049136292
-
-
V. Schmitt, F. Charpin, Pressure distributions on the ONERA-M6-wing at transonic Mach numbers, AGARD Advisory Report No. 138, 1979, pp. B1-1-B1-44
-
V. Schmitt, F. Charpin, Pressure distributions on the ONERA-M6-wing at transonic Mach numbers, AGARD Advisory Report No. 138, 1979, pp. B1-1-B1-44
-
-
-
-
21
-
-
55049085725
-
-
V. Schmitt, J. Cousteix, Étude de la couche limite tridimensionelle sur une aile en flèche, ONERA, Rapport Technique No 14/1713 AN, Châtillon, France, July 1975
-
V. Schmitt, J. Cousteix, Étude de la couche limite tridimensionelle sur une aile en flèche, ONERA, Rapport Technique No 14/1713 AN, Châtillon, France, July 1975
-
-
-
-
22
-
-
55049113714
-
-
G. Schrauf, LILO 2.1 user's guide and tutorial, Bremen, Germany, GSSC Technical Report 6, originally issued Sep. 2004, modified for Version 2.1 July 2006
-
G. Schrauf, LILO 2.1 user's guide and tutorial, Bremen, Germany, GSSC Technical Report 6, originally issued Sep. 2004, modified for Version 2.1 July 2006
-
-
-
-
23
-
-
55049090355
-
-
G. Schrauf, Transition prediction using different linear stability analysis strategies, AIAA Paper 1994-1848, June 1994
-
G. Schrauf, Transition prediction using different linear stability analysis strategies, AIAA Paper 1994-1848, June 1994
-
-
-
-
24
-
-
55049124485
-
-
A.M.O. Smith, N. Gamberoni, Transition, pressure gradient and stability theory, Douglas Aircraft Company, Long Beach, Calif. Rep. ES 26388, 1956
-
A.M.O. Smith, N. Gamberoni, Transition, pressure gradient and stability theory, Douglas Aircraft Company, Long Beach, Calif. Rep. ES 26388, 1956
-
-
-
-
25
-
-
20444482119
-
N transition prediction
-
N transition prediction. AIAA Journal 43 5 (June 1989) 1221-1229
-
(1989)
AIAA Journal
, vol.43
, Issue.5
, pp. 1221-1229
-
-
Stock, H.W.1
-
27
-
-
0032595442
-
N transition prediction in Navier-Stokes methods for airfoils
-
N transition prediction in Navier-Stokes methods for airfoils. AIAA Journal 37 10 (1999) 1187-1196
-
(1999)
AIAA Journal
, vol.37
, Issue.10
, pp. 1187-1196
-
-
Stock, H.W.1
Haase, W.2
-
28
-
-
55049110552
-
-
J.L. van Ingen, A suggested semi-empirical method for the calculation of the boundary layer transition region, University of Delft, Dept. of Aerospace Engineering, Delft, The Netherlands, Rep. VTH-74, 1956
-
J.L. van Ingen, A suggested semi-empirical method for the calculation of the boundary layer transition region, University of Delft, Dept. of Aerospace Engineering, Delft, The Netherlands, Rep. VTH-74, 1956
-
-
-
-
29
-
-
0032154108
-
Transition closure model for predicting transition onset
-
Warren E.S., and Hassan H.A. Transition closure model for predicting transition onset. Journal of Aircraft 35 (1998) 769-775
-
(1998)
Journal of Aircraft
, vol.35
, pp. 769-775
-
-
Warren, E.S.1
Hassan, H.A.2
|