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Results:
1-22
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Results: 22
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:
Chong, YH
Imregun, M
Citation: Yh. Chong et M. Imregun, Development and application of a nonlinear modal analysis technique for MDOF systems, J VIB CONTR, 7(2), 2001, pp. 167-179
Authors:
Zang, C
Imregun, M
Citation: C. Zang et M. Imregun, Combined neural network and reduced FRF techniques for slight damage detection using measured response data, ARCH APPL M, 71(8), 2001, pp. 525-536
Authors:
Sbardella, L
Imregun, M
Citation: L. Sbardella et M. Imregun, Linearized unsteady viscous turbomachinery flows using hybrid grids, J TURBOMACH, 123(3), 2001, pp. 568-582
Authors:
Zang, C
Grafe, H
Imregun, M
Citation: C. Zang et al., Frequency-domain criteria for correlating and updating dynamic finite element models, MECH SYST S, 15(1), 2001, pp. 139-155
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:
Zang, C
Imregun, M
Citation: C. Zang et M. Imregun, Structural damage detection using artificial neural networks and measured FRF data reduced via principal component protection, J SOUND VIB, 242(5), 2001, pp. 813-827
Authors:
Sbardella, L
Tester, BJ
Imregun, M
Citation: L. Sbardella et al., A time-domain method for the prediction of sound attenuation in lined ducts, J SOUND VIB, 239(3), 2001, pp. 379-396
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:
Chong, YH
Imregun, M
Citation: Yh. Chong et M. Imregun, Variable modal parameter identification for non-linear mdof systems. Part I: Formulation and numerical validation, SHOCK VIB, 7(4), 2000, pp. 217-227
Authors:
Chong, YH
Imregun, M
Citation: Yh. Chong et M. Imregun, Variable modal parameter identification for non-linear mdof systems. Part II: Experimental validation and advanced case study, SHOCK VIB, 7(4), 2000, pp. 229-240
Authors:
Sbardella, L
Imregun, M
Citation: L. Sbardella et M. Imregun, An efficient discretization of viscous fluxes on unstructured mixed-element grids, COMMUN NUM, 16(12), 2000, pp. 839-849
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:
Chong, YH
Imregun, M
Citation: Yh. Chong et M. Imregun, Use of reciprocal modal vectors for nonlinearity detection, ARCH APPL M, 70(7), 2000, pp. 453-462
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:
Chong, YH
Imregun, M
Citation: Yh. Chong et M. Imregun, Coupling of non-linear substructures using variable modal parameters, MECH SYST S, 14(5), 2000, pp. 731-746
Authors:
Sbardella, L
Sayma, AI
Imregun, M
Citation: L. Sbardella et al., Semi-structured meshes for axial turbomachinery blades, INT J NUM F, 32(5), 2000, pp. 569-584
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:
Ziaei-Rad, S
Imregun, M
Citation: S. Ziaei-rad et M. Imregun, On the use of regularisation techniques for finite element model updating, INVERSE P E, 7(5), 1999, pp. 471-503
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
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