-
1
-
-
0028372478
-
Simulation of Transition with a Two-Equation Turbulence Model
-
Feb
-
Wilcox, D., "Simulation of Transition with a Two-Equation Turbulence Model," AIAA Journal, Vol. 32, Feb. 1994, pp. 247-255.
-
(1994)
AIAA Journal
, vol.32
, pp. 247-255
-
-
Wilcox, D.1
-
2
-
-
34250837287
-
Transition Modeling Based on Local Variables
-
Menter, F., Esch, T., and Kubacki, S., "Transition Modeling Based on Local Variables," 5th International Symposium on Engineering Turbulence Modelling and Measurements, 2002.
-
(2002)
5th International Symposium on Engineering Turbulence Modelling and Measurements
-
-
Menter, F.1
Esch, T.2
Kubacki, S.3
-
3
-
-
10244225305
-
A Correlation-Based Transition Model, using Local Variables Part 2: Model Formulation
-
American Society of Mechanical Engineers
-
Menter, F., Langtry, R., Likki, S., Suzen, Y., Huang, P., and Völker, S., "A Correlation-Based Transition Model, using Local Variables Part 2: Model Formulation," ASME Turbo Expo 2004 Power for Land, See and Air, American Society of Mechanical Engineers GT2004-53452, 2004.
-
ASME Turbo Expo 2004 Power for Land, See and Air
, vol.GT2004-53452
, pp. 2004
-
-
Menter, F.1
Langtry, R.2
Likki, S.3
Suzen, Y.4
Huang, P.5
Völker, S.6
-
4
-
-
10244245023
-
A Correlation-Based Transition Model Using Local Variables Part 2: Test Cases and Industrial Applications
-
American Society of Mechanical Engineers
-
Langtry, R., Menter, F., Likki, S., Suzen, Y., Huang, P., and Völker, S., "A Correlation-Based Transition Model Using Local Variables Part 2: Test Cases and Industrial Applications," ASME Turbo Expo 2004 Power for Land, See and Air, American Society of Mechanical Engineers, GT2004-53454, 2004.
-
ASME Turbo Expo 2004 Power for Land, See and Air
, vol.GT2004-53454
, pp. 2004
-
-
Langtry, R.1
Menter, F.2
Likki, S.3
Suzen, Y.4
Huang, P.5
Völker, S.6
-
5
-
-
30744468823
-
Transition Modeling for General CFD Applications in Aeronautics
-
AIAA Paper 2005-522
-
Langtry, R., and Menter, F., "Transition Modeling for General CFD Applications in Aeronautics," AIAA Paper 2005-522, 2005.
-
(2005)
-
-
Langtry, R.1
Menter, F.2
-
6
-
-
85086614602
-
-
Krumbein, A., On Modeling of Transitional Flow and its Application on a High Lift Multi-Element Airfoil Configuration, 41st Aerospace Sciences Meeting and Exhibit, AIAA 2003-724, Jan. 2003.
-
Krumbein, A., "On Modeling of Transitional Flow and its Application on a High Lift Multi-Element Airfoil Configuration," 41st Aerospace Sciences Meeting and Exhibit, AIAA 2003-724, Jan. 2003.
-
-
-
-
8
-
-
2942752279
-
Overview About the European High Lift Research Programme EUROLIFT, 42nd AIAA Aerospace Sciences Meeting and Exhibit
-
AIAA Paper 2004-767, Jan
-
Hansen, H., Thiede, P., Rudnik, R., Moens, F., and Quest, J., "Overview About the European High Lift Research Programme EUROLIFT," 42nd AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2004-767, Jan. 2004.
-
(2004)
-
-
Hansen, H.1
Thiede, P.2
Rudnik, R.3
Moens, F.4
Quest, J.5
-
9
-
-
85088183530
-
elsA: An Efficient Object-Oriented Solution to CFD Complexity
-
AIAA Paper 2002-0108, Jan
-
Cambier, L., and Gazaix, M., "elsA: An Efficient Object-Oriented Solution to CFD Complexity," 40th AIAA Aerospace Sciences Meeting & Exhibit, AIAA Paper 2002-0108, Jan. 2002.
-
(2002)
40th AIAA Aerospace Sciences Meeting & Exhibit
-
-
Cambier, L.1
Gazaix, M.2
-
10
-
-
0032595442
-
N Transition Prediction Method in Navier-Stokes Methods for Airfoils
-
N Transition Prediction Method in Navier-Stokes Methods for Airfoils," AIAA Journal, Vol. 37, No. 10, 1999, pp. 1187-1196.
-
(1999)
AIAA Journal
, vol.37
, Issue.10
, pp. 1187-1196
-
-
Stock, H.1
andHaase, W.2
-
11
-
-
44849113033
-
-
Douglas Aircraft Co, Rept
-
Smith, A. M. O., and Gamberoni, N., "Transition, Pressure Gradient and Stability Theory," Douglas Aircraft Co., Rept. ES 26 388, 1956.
-
(1956)
Transition, Pressure Gradient and Stability Theory
, vol.ES 26
, pp. 388
-
-
Smith, A.M.O.1
Gamberoni, N.2
-
12
-
-
44849138312
-
-
van Ingen, J. L., A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region, Delft Univ. of Technology, Dept. of Aeronautic Engineering, Rept. UTH-74, Delft, The Netherlands, 1956.
-
van Ingen, J. L., "A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region," Delft Univ. of Technology, Dept. of Aeronautic Engineering, Rept. UTH-74, Delft, The Netherlands, 1956.
-
-
-
-
14
-
-
44849099772
-
-
Arnal, D., Special Course on Stability and Transition of Laminar Flow, AGARD Special Course at the von Kármán Inst., AGARD Rept. No. 709, 26-30 March 1984.
-
Arnal, D., "Special Course on Stability and Transition of Laminar Flow," AGARD Special Course at the von Kármán Inst., AGARD Rept. No. 709, 26-30 March 1984.
-
-
-
-
15
-
-
0008846583
-
Calculation of the Viscous Drag of Bodies of Revolution
-
Granville, P. S., "Calculation of the Viscous Drag of Bodies of Revolution," David Taylor Model Basin Rept. 849, 1953.
-
(1953)
David Taylor Model Basin Rept
, vol.849
-
-
Granville, P.S.1
-
16
-
-
4243159708
-
Theoretical and Experimental Study of Low Reynolds Number Transitional Separation Bubbles
-
Univ. of Notre Dame, Notre Dame, IN
-
Gleyzes, C., Cousteix, J., and Bonnet, J. L., "Theoretical and Experimental Study of Low Reynolds Number Transitional Separation Bubbles," Conference on Low Reynolds N umber Airfoil Aerodynamics, Univ. of Notre Dame, Notre Dame, IN, 1985.
-
(1985)
Conference on Low Reynolds N umber Airfoil Aerodynamics
-
-
Gleyzes, C.1
Cousteix, J.2
Bonnet, J.L.3
-
17
-
-
44849118023
-
-
Habiballah, M., Analyse de l'instabilité des Couches Limites Laminaires et Prévision de la Transition du Régime Laminaire au Régime Turbulent, Ph.D. Thesis, École Nationale Supérieure de l'Aéronautique et de l'Espace, Toulouse, France, June 1981.
-
Habiballah, M., "Analyse de l'instabilité des Couches Limites Laminaires et Prévision de la Transition du Régime Laminaire au Régime Turbulent," Ph.D. Thesis, École Nationale Supérieure de l'Aéronautique et de l'Espace, Toulouse, France, June 1981.
-
-
-
-
19
-
-
34250869950
-
Numerical Simulation of Three-Dimensional Supersonic Flows Using Euler and Boundary-Layer Solvers
-
AIAA 93-0531, Jan
-
Gaible, F., Cariou, R., and Houdeville, R., "Numerical Simulation of Three-Dimensional Supersonic Flows Using Euler and Boundary-Layer Solvers," 31th AIAA Aerospace Sciences Meeting & Exhibit, AIAA 93-0531, Jan. 1997.
-
(1997)
31th AIAA Aerospace Sciences Meeting & Exhibit
-
-
Gaible, F.1
Cariou, R.2
Houdeville, R.3
-
21
-
-
44849086272
-
-
Manie, F., Piccin, O., and Ray, J., Test Report of the 2-D Model M1 in the ONERA F1 Wind Tunnel, Group for Aeronautical Research and Technology in Europe High-Lift Action Group AD (AG-08),TP041, Oct. 1989.
-
Manie, F., Piccin, O., and Ray, J., "Test Report of the 2-D Model M1 in the ONERA F1 Wind Tunnel," Group for Aeronautical Research and Technology in Europe High-Lift Action Group AD (AG-08),TP041, Oct. 1989.
-
-
-
-
22
-
-
78649459961
-
Application of Transition Criteria in Navier-Stokes Computations
-
Jan
-
Arthur, M., Dol, H., Krumbein, A., Houdeville, R., and Ponsin, J., "Application of Transition Criteria in Navier-Stokes Computations," GARTEUR TP-137, Jan. 2003.
-
(2003)
GARTEUR TP-137
-
-
Arthur, M.1
Dol, H.2
Krumbein, A.3
Houdeville, R.4
Ponsin, J.5
-
23
-
-
0013124137
-
Near Wall Model, for the k - 1 Two Equation Turbulence Model
-
AIAA Paper 94-2386, June
-
Smith, B., "Near Wall Model, for the k - 1 Two Equation Turbulence Model," 25th Fluid Dynamics Conference, AIAA Paper 94-2386, June 1994.
-
(1994)
25th Fluid Dynamics Conference
-
-
Smith, B.1
-
24
-
-
7544226293
-
Transition Prediction in Transonic Flow
-
Springer-Verlag, Berlin
-
Arnal, D., "Transition Prediction in Transonic Flow," IUTAM Symposium Transsonicum III DFVLR-AVA, Springer-Verlag, Berlin, 1988, pp. 253-262.
-
(1988)
IUTAM Symposium Transsonicum III DFVLR-AVA
, pp. 253-262
-
-
Arnal, D.1
-
25
-
-
0346724397
-
-
Séraudie, A., Penaud, J., and Moens, F., 'Transition Measurements and Analysis on a Swept Wing in High-Lift Configuration, Aerospace Science and Technology, 7, No. 8, 2003, pp. 569-576. doi:10.1016/j.ast.2003.04.001
-
Séraudie, A., Penaud, J., and Moens, F., 'Transition Measurements and Analysis on a Swept Wing in High-Lift Configuration," Aerospace Science and Technology, Vol. 7, No. 8, 2003, pp. 569-576. doi:10.1016/j.ast.2003.04.001
-
-
-
-
26
-
-
7544232510
-
Transition on a High-Lift Swept Wing in the European Project EUROLIFT
-
Perraud, J., Séraudie, A., and Moens, F., "Transition on a High-Lift Swept Wing in the European Project EUROLIFT," Journal of Aircraft, Vol. 41, No. 5, 2004, pp. 1183-1190.
-
(2004)
Journal of Aircraft
, vol.41
, Issue.5
, pp. 1183-1190
-
-
Perraud, J.1
Séraudie, A.2
Moens, F.3
-
27
-
-
34347223597
-
Automatic Transition Prediction for RANS Computations Applied to a Generic High-Lift Wing
-
AIAA 07-1086
-
Toulorge, T., Ponsin, J., Perraud, J., and Moens, F., "Automatic Transition Prediction for RANS Computations Applied to a Generic High-Lift Wing," 45th AIAA Aerospace Sciences Meeting & Exhibit, AIAA 07-1086, 2007.
-
(2007)
45th AIAA Aerospace Sciences Meeting & Exhibit
-
-
Toulorge, T.1
Ponsin, J.2
Perraud, J.3
Moens, F.4
|