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Results:
1-9
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Results: 9
Authors:
Kim, M
Vahdati, M
Imregun, M
Citation: M. Kim et al., Aeroelastic stability analysis of a bird-damaged aeroengine fan assembly, AEROSP SC T, 5(7), 2001, pp. 469-482
Authors:
Vahdati, M
Sayma, AI
Marshall, JG
Imregun, M
Citation: M. Vahdati et al., Mechanisms and prediction methods for fan blade stall flutter, J PROPUL P, 17(5), 2001, pp. 1100-1108
Authors:
Breard, C
Green, JS
Vahdati, M
Imregun, M
Citation: C. Breard et al., A non-linear integrated aeroelasticity method for the prediction of turbine forced response with friction dampers, INT J MECH, 43(12), 2001, pp. 2715-2736
Authors:
Sayma, AI
Vahdati, M
Imregun, M
Citation: Ai. Sayma et al., Multi-bladerow fan forced response predictions using an integrated three-dimensional time-domain aeroelasticity model, P I MEC E C, 214(12), 2000, pp. 1467-1483
Authors:
Sayma, AI
Vahdati, M
Imregun, M
Citation: Ai. Sayma et al., An integrated nonlinear approach for turbomachinery forced response prediction. Part I: Formulation, J FLUID STR, 14(1), 2000, pp. 87-101
Authors:
Vahdati, M
Sayma, AI
Imregun, M
Citation: M. Vahdati et al., An integrated nonlinear approach for turbomachinery forced response prediction. Part II: Case studies, J FLUID STR, 14(1), 2000, pp. 103-125
Authors:
Sayma, AI
Vahdati, M
Sbardella, L
Imregun, M
Citation: Ai. Sayma et al., Modeling of three-dimensional viscous compressible turbomachinery flows using unstructured hybrid grids, AIAA J, 38(6), 2000, pp. 945-954
Authors:
Imregun, M
Vahdati, M
Citation: M. Imregun et M. Vahdati, Aeroelasticity analysis of a bird-damaged fan assembly using a large numerical model, AERONAUT J, 103(1030), 1999, pp. 569-578
Authors:
Sayma, AI
Vahdati, M
Imregun, M
Green, JS
Citation: Ai. Sayma et al., Whole-assembly flutter analysis of a low-pressure turbine blade, AERONAUT J, 102(1018), 1998, pp. 459-463
Risultati:
1-9
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