1 |
Wu, X, Vahdati, Sayma, A. and Imregun, M., 'Whole-annulus aeroelasticity analysis of a 17-bladerow WRF compressor using an unstructured Navier- Stokes solver,' Intemational Journal of Computational Fluid Dynamics, Vol. 19, No. 3, 2005, pp. 211-223
DOI
ScienceOn
|
2 |
Sadeghi, M. and Liu, F., 'Investigation of Mistuning Effects on Cascade Flutter Using a Coupled Method,' J. of Propulsion and Power, Vol. 23, No. 2, 2007, pp
266- 274
DOI
ScienceOn
|
3 |
He, Z. and Epureanu, B.I., 'FIuid-Structural Coupling Effects on the Dynamics of Mistuned Bladed Disks,' AIAA Journal, Vol. 45, No. 3, 2007, pp. 552-561
DOI
ScienceOn
|
4 |
Namkoong, K., Choi, H.G., and Yoo, J.Y., 'Computation of dynamic fluid-structure interaction in two-dimensional laminar flows using combined formulation,' J. of Fluids and Structures, Vol. 20, 2005, pp. 51-69
DOI
ScienceOn
|
5 |
Huff, D. L. and Reddy, T. S. R., 'Numerical Analysis of Supersonic Flow Through Oscillating Cascade Sections by Using a Defornllng Grid,' AIAA Paper 89-2805, 1989
|
6 |
Eick, C. D., and Liu, J. S., 'Comparisons of Aeroelastic Computer Code Predictions Against Measured Rotor Vibratory Response Data,' AIAA paper 97-2750, 1997
|
7 |
Gao., c., Luo, S., and Liu, F., 'Calculation of Airfoil Flutter by an Euler Method with Approximate Boundary Conditions,' AlAA paper 2003-3830, 16th AlAA Computational Fluid Dynamics Conference, June 23-26, 2003
|
8 |
Bendiksen, O. O., 'A New Approach to Computational Aeroelasticity,' AIAA paper 91- 0939, 1991
|
9 |
Masud, A., 'A Space-Time Finite Element Formulation for Fluid-Structure Interaction,' AIAA paper 96-4049, 6th AIAA Symposium on Multidisciplinary Analysis and Optimization, September 4-6, 1996
|
10 |
Gottfried, D. A., and Fleeter, S., 'Prediction of Unsteady Cascade Aerodynamics by an Arbitrary Lagrangian Eulerian Finite Element Method,', AIAA paper 98-374,
1998
|
11 |
Gottfried, D. A., and Fleeter, S., 'Turbomachinery Blade Row Interaction Predictions with a Three-Dimensional Finite Element Method,' AIAA paper 2000-3226, 2000
|
12 |
Breard, C., Imregun, M., Sayma, A., and Vahdati, M., 'Flutter Stability Analysis of a Complete Fan Assembly,' AIAA paper 99 -238,37th AIAA Aerospace Sciences Meeting and Exhibit, January 11-14, 1999
|
13 |
Servera, G., Beaumier, P., and Costes, M., 'A Weak Coupling Method Between the Dynamic Code HOST and the 3D Unsteady Euler Code W A VES,' Journal of Aerospace, Science and Technology, Vol. 5, 2001, pp. 397-408
DOI
ScienceOn
|
14 |
Carstens, V., Kemme, R., and Schmitt, S., 'Coupled Simulation of Flow-structure Interaction in Turbomachinery,' Journal of Aerospace Science and Technology, Vol. 7, Issue 4, 2003, pp. 298-306
DOI
ScienceOn
|
15 |
Gerolymos, G. A., 'Numerical Integration of the 3D Unsteady Euler Equations for Flutter Analysis of Axial Flow Compressors,' ASME paper 88-GT-255,1988
|
16 |
Marshall,J. G., and Imregun, M., 'A Review of Aeroelasticity Methods with Emphasis on Turbomachinery Applications,' Journal of Fluids and Structures, Vol. 10, Issue 3, April 1996, pp. 237-267
DOI
ScienceOn
|
17 |
Lane, F., 'System Mode Shapes in the Flutter of Compressor Blade Rows,' Journal of Aeronautical Sciences, Vol. 23, 1956, pp. 54-66
DOI
|
18 |
Whitehead, D. S., 'Classical Two- Dimensional Methods, In Aeroelasticity in Axial-F1ow Turbomachines,' AGARD Manual on Aeroelasticity in Turbomachines, AGARDAG- 298, Vol. 1, Unsteady Turbomachinery Aerodynamics, 1989
|
19 |
Wolff, J. M., and Fleeter, S., 'Euler Analysis of Oscillating Cascade Unsteady Aerodynamics Using Embedded Composite Grids,' AIAA paper 94-0077, 1994
|
20 |
Ji, S. and Liu, F., 'Computation of Unsteady Flows Around Oscillating Blades and Aeroelasticity Behavior,' AIAA paper 97-0161, 35th AIAA Aerospace Sciences Meeting and Exhibit,January 6-9, 1997, Reno, NV
|
21 |
Weber, S., Gallus, H. E., and Peitsch, D., 'A Numerical Approach to Unstalled and Stalled Flutter Phenomena in Turbomachinery,' ASME paper 97-GT-102, 1997
|