-
1
-
-
0346753316
-
-
Sept., Harrogate, UK
-
Joubert, H., and Quiniou, H., 2000, "Turbomachinery Design Used Intensive CFD 22nd ICAS," Sept., Harrogate, UK.
-
(2000)
Turbomachinery Design Used Intensive CFD 22nd ICAS
-
-
Joubert, H.1
Quiniou, H.2
-
4
-
-
85086614356
-
Multidisciplinary aerodynamic-structural shape optimization using deformation (MASSOUD)
-
Sept. 6-8, Long Beach, CA
-
Samareh, Jamshid A., 2000, "Multidisciplinary Aerodynamic-Structural Shape Optimization Using Deformation (MASSOUD ," 8th AIAA/NASA/USAF/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Sept. 6-8, Long Beach, CA.
-
(2000)
8th AIAA/NASA/USAF/ISSMO Symposium on Multidisciplinary Analysis and Optimization
-
-
Samareh, J.A.1
-
6
-
-
1942535604
-
The use of bézier polynomial patches to define geometrical shape of the flow channels of compressors
-
Quinhuan, W., and Xiaoyan, H., 1988, "The Use of Bézier Polynomial Patches to Define Geometrical Shape of the Flow Channels of Compressors," ASME Paper 88-GT-60.
-
(1988)
ASME Paper 88-GT-60
-
-
Quinhuan, W.1
Xiaoyan, H.2
-
7
-
-
1942503804
-
-
ISABE2001-1117, Sept. 2-7, Bangalore
-
Burguburu, S., Toussaint, C., and Leroy, G., 2001, "Numerical Optimization for Turbomachinery Blades Aerodynamic Design Using a Gradient Method Coupled With a Navier-Stokes Solver 15th ISABE," ISABE2001-1117, Sept. 2-7, Bangalore.
-
(2001)
Numerical Optimization for Turbomachinery Blades Aerodynamic Design Using a Gradient Method Coupled With a Navier-Stokes Solver 15th ISABE
-
-
Burguburu, S.1
Toussaint, C.2
Leroy, G.3
-
9
-
-
84982318310
-
Numerical simulation of separated turbulent flows based on the solution of a RANS/low reynolds two-equations model
-
Reno NV
-
Couailler, V., 1999, "Numerical Simulation of Separated Turbulent Flows Based on the Solution of a RANS/Low Reynolds Two-Equations Model," 37th AIAA/ASME, Reno NV.
-
(1999)
37th AIAA/ASME
-
-
Couailler, V.1
-
10
-
-
0004065720
-
-
Technical Note 154, Office National d'Etudes et Recherches Aérospatiales
-
Michel, R., Quémard, C., and Durand, R., 1969, "Application d'un schéma de longueur de mélange à l'étude des couches limites turbulentes d'équilibre," Technical Note 154, Office National d'Etudes et Recherches Aérospatiales.
-
(1969)
Application D'un Schéma de Longueur de Mélange à L'étude Des Couches Limites Turbulentes D'équilibre
-
-
Michel, R.1
Quémard, C.2
Durand, R.3
-
11
-
-
84890233725
-
Shape optimization of transonic compressor blades using quasi-3D flow physics
-
Chung, J., and Lee, K. D., 2000, "Shape Optimization of Transonic Compressor Blades Using Quasi-3D Flow Physics," ASME Paper 2000-GT-0489.
-
(2000)
ASME Paper 2000-GT-0489
-
-
Chung, J.1
Lee, K.D.2
-
12
-
-
84955473748
-
Using sweep and dihedral to control three-dimensional flow in transonic stator of axial compressor
-
Gummer, V., Wenger, U., and Kau, H. P., 2000, "Using Sweep and Dihedral to Control Three-Dimensional Flow in Transonic Stator of Axial Compressor," ASME Paper 2000-GT-0491.
-
(2000)
ASME Paper 2000-GT-0491
-
-
Gummer, V.1
Wenger, U.2
Kau, H.P.3
-
13
-
-
1942471545
-
-
15th ISABE, ISABE2001-1053, Sept. 2-7, Bangalore
-
Shaphar, S., 2001, "Three-Dimensional Design and Optimization of Turbomachinery Blades Using the Navier-Stokes Equations," 15th ISABE, ISABE2001-1053, Sept. 2-7, Bangalore.
-
(2001)
Three-Dimensional Design and Optimization of Turbomachinery Blades Using the Navier-Stokes Equations
-
-
Shaphar, S.1
-
14
-
-
84885276174
-
3D design of transonic axial compressor blades with 3D navier-stokes physics
-
Chung, J., Shim, J., and Lee, K. D., 2001, "3D Design of Transonic Axial Compressor Blades With 3D Navier-Stokes Physics," AIAA Paper 2001-3305.
-
(2001)
AIAA Paper 2001-3305
-
-
Chung, J.1
Shim, J.2
Lee, K.D.3
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