-
1
-
-
0022693320
-
Forced Response Analysis of an Aerodynamically Detuned Supersonic Turbomachine Rotor
-
Fleeter, S., and Hoyniak, D., 1986, "Forced Response Analysis of an Aerodynamically Detuned Supersonic Turbomachine Rotor," ASME J. Vib., Acoust., Stress, Reliab. Des., 108(2), pp. 117-124.
-
(1986)
ASME J. Vib., Acoust., Stress, Reliab. Des
, vol.108
, Issue.2
, pp. 117-124
-
-
Fleeter, S.1
Hoyniak, D.2
-
2
-
-
0022440305
-
Aerodynamic Detuning Analysis of an Unstalled Supersonic Turbofan Cascade
-
Fleeter, S., and Hoyniak, D., 1986, "Aerodynamic Detuning Analysis of an Unstalled Supersonic Turbofan Cascade," ASME J. Eng. Gas Turbines Power, 108(1), pp. 60-67.
-
(1986)
ASME J. Eng. Gas Turbines Power
, vol.108
, Issue.1
, pp. 60-67
-
-
Fleeter, S.1
Hoyniak, D.2
-
4
-
-
0036648918
-
The Effect of Variable Chord Length on Transonic Axial Rotor Performance
-
Roberts, W. B., Armin, A., Kassaseya, G., Suder, K. L., Thorp, S. A., and Strazisar, A. J., 2002, "The Effect of Variable Chord Length on Transonic Axial Rotor Performance," ASME J. Turbomach., 124(3), pp. 351-357.
-
(2002)
ASME J. Turbomach
, vol.124
, Issue.3
, pp. 351-357
-
-
Roberts, W.B.1
Armin, A.2
Kassaseya, G.3
Suder, K.L.4
Thorp, S.A.5
Strazisar, A.J.6
-
5
-
-
0032638012
-
3D-Shock Visualisation in a Transonic Compressor Rotor
-
Roehle, I., Le Guevel, A., and Fradin, C., 1999, "3D-Shock Visualisation in a Transonic Compressor Rotor," Opt. Laser Technol., 31(1), pp. 67-73.
-
(1999)
Opt. Laser Technol
, vol.31
, Issue.1
, pp. 67-73
-
-
Roehle, I.1
Le Guevel, A.2
Fradin, C.3
-
6
-
-
15344349684
-
Fluid-Structure Interaction for Aeroelastic Applications
-
Kamakoti, R., and Shyy, W., 2004, "Fluid-Structure Interaction for Aeroelastic Applications," Prog. Aesosp. Sci., 40, pp. 535-558.
-
(2004)
Prog. Aesosp. Sci
, vol.40
, pp. 535-558
-
-
Kamakoti, R.1
Shyy, W.2
-
7
-
-
0026836987
-
Structural and Aerodynamic Analysis of a Large-Scale Advanced Propeller Blade
-
Yamamoto, O., and August, R., 1992, "Structural and Aerodynamic Analysis of a Large-Scale Advanced Propeller Blade," J. Propul. Power, 8(2), pp. 367-373.
-
(1992)
J. Propul. Power
, vol.8
, Issue.2
, pp. 367-373
-
-
Yamamoto, O.1
August, R.2
-
8
-
-
0026223272
-
Application of an Efficient Hybrid Scheme for Aeroelastic Analysis of Advanced Propellers
-
Srivastava, R., Sankar, L. N., Reddy, T. S. R., and Huff, D. L., 1991, "Application of an Efficient Hybrid Scheme for Aeroelastic Analysis of Advanced Propellers," J. Propul. Power, 7(5), pp. 767-775.
-
(1991)
J. Propul. Power
, vol.7
, Issue.5
, pp. 767-775
-
-
Srivastava, R.1
Sankar, L.N.2
Reddy, T.S.R.3
Huff, D.L.4
-
9
-
-
0024673739
-
Integrated Approach for Active Coupling of Fluids and Structures
-
Guruswamy, G. P., 1989, "Integrated Approach for Active Coupling of Fluids and Structures," AIAA J., 27(6), pp. 788-793.
-
(1989)
AIAA J
, vol.27
, Issue.6
, pp. 788-793
-
-
Guruswamy, G.P.1
-
10
-
-
34249894758
-
-
Marshall, J. G., 1996, Prediction of Turbomachinery Aeroelasticity Effects Using a 3D Nonlinear Integrated Method, Ph.D. thesis, Imperial College of Science, Technology and Medicine, University of London.
-
Marshall, J. G., 1996, "Prediction of Turbomachinery Aeroelasticity Effects Using a 3D Nonlinear Integrated Method," Ph.D. thesis, Imperial College of Science, Technology and Medicine, University of London.
-
-
-
-
11
-
-
0003206778
-
An Integrated Non-Linear Approach for Turbomachinery Forced Response prediction - Part 1: Formulation
-
Sayma, A. I., Vahdati, M., and Imregun, M., 2000, "An Integrated Non-Linear Approach for Turbomachinery Forced Response prediction - Part 1: Formulation," J. Fluids Struct., 14(1), pp. 87-101.
-
(2000)
J. Fluids Struct
, vol.14
, Issue.1
, pp. 87-101
-
-
Sayma, A.I.1
Vahdati, M.2
Imregun, M.3
-
12
-
-
0033729894
-
Modelling of 3D Viscous Compressible Turbomachinery Flows Using Unstructured Hybrid Grids
-
Sayma, A. I., Vahdati, M., Sbardella, L., and Imregun, M., 2000, "Modelling of 3D Viscous Compressible Turbomachinery Flows Using Unstructured Hybrid Grids," AIAA J., 38(6), pp. 945-954.
-
(2000)
AIAA J
, vol.38
, Issue.6
, pp. 945-954
-
-
Sayma, A.I.1
Vahdati, M.2
Sbardella, L.3
Imregun, M.4
-
13
-
-
0034652815
-
Semi-Unstructured Meshes for Axial Turbomachine Blades
-
Sbardella, L., Sayma, A. I., and Imregun, M., 2000, "Semi-Unstructured Meshes for Axial Turbomachine Blades," Int. J. Numer. Methods Fluids, 32(5), pp. 569-584.
-
(2000)
Int. J. Numer. Methods Fluids
, vol.32
, Issue.5
, pp. 569-584
-
-
Sbardella, L.1
Sayma, A.I.2
Imregun, M.3
-
15
-
-
0026118616
-
Unsteady Euler Algorithm With Unstructured Dynamic Mesh for Complex-Aircraft Aerodynamic Analysis
-
Batina, J. T., 1991, "Unsteady Euler Algorithm With Unstructured Dynamic Mesh for Complex-Aircraft Aerodynamic Analysis," AIAA J., 29(3), pp. 327-333.
-
(1991)
AIAA J
, vol.29
, Issue.3
, pp. 327-333
-
-
Batina, J.T.1
-
16
-
-
0026261105
-
Aeroelastic Analysis of Wings Using the Euler Equations With a Deforming Mesh
-
Robinson, B. A., Batina, J. T., and Yang, H. T. Y., 1991, "Aeroelastic Analysis of Wings Using the Euler Equations With a Deforming Mesh," J. Aircr., 28(11), pp. 781-788.
-
(1991)
J. Aircr
, vol.28
, Issue.11
, pp. 781-788
-
-
Robinson, B.A.1
Batina, J.T.2
Yang, H.T.Y.3
-
17
-
-
32044473950
-
The Effect of Stagger Variability in Gas Turbine Fan Assemblies
-
Sept. 4-7, Institution of Mechanical Engineers, pp
-
Wilson, M. J., Imregun, M., and Sayma, A. I., 2005, "The Effect of Stagger Variability in Gas Turbine Fan Assemblies," International Conference on Compressors and Their Systems, Sept. 4-7, Institution of Mechanical Engineers, pp. 507-515.
-
(2005)
International Conference on Compressors and Their Systems
, pp. 507-515
-
-
Wilson, M.J.1
Imregun, M.2
Sayma, A.I.3
-
18
-
-
0035299034
-
Numerical Investigation of Nonlinear Fluid-Structure Interaction in Vibrating Compressor Blades
-
Carstens, V., and Belz, J., 2001, "Numerical Investigation of Nonlinear Fluid-Structure Interaction in Vibrating Compressor Blades," ASME J. Turbomach., 123(2), pp. 402-408.
-
(2001)
ASME J. Turbomach
, vol.123
, Issue.2
, pp. 402-408
-
-
Carstens, V.1
Belz, J.2
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