A survey of nonlinear analysis tools for structural systemsIMREGUN, M.The Shock and vibration digest. 1998, Vol 30, Num 5, pp 363-369, issn 0583-1024Article

Prediction of flutter stability using aerolastic frequency response functionsIMREGUN, M.Journal of fluids and structures. 1995, Vol 9, Num 4, pp 419-434, issn 0889-9746Article

Aeroelasticity analysis of a bird-damaged fan assembly using a large numerical modelIMREGUN, M; VAHDATI, M.Aeronautical Journal. 1999, Vol 103, Num 1030, pp 569-578, issn 0001-9240Article

On the accuracy required of experimental data for finite element model updatingZIAEI-RAD, S; IMREGUN, M.Journal of sound and vibration. 1996, Vol 196, Num 3, pp 323-336, issn 0022-460XArticle

An explicit frequency response function formulation for multi-degree-of-freedom non-linear systemsELIZALDE, H; IMREGUN, M.Mechanical systems and signal processing. 2006, Vol 20, Num 8, pp 1867-1882, issn 0888-3270, 16 p.Article

Use of reciprocal modal vectors for nonlinearity detectionCHONG, Y. H; IMREGUN, M.Archive of applied mechanics (1991). 2000, Vol 70, Num 7, pp 453-462, issn 0939-1533Article

An improved single-parameter tip-timing method for turbomachinery blade vibration measurements using optical laser probesHEATH, S; IMREGUN, M.International journal of mechanical sciences. 1996, Vol 38, Num 10, pp 1047-1058, issn 0020-7403Article

A non-linear aeroelasticity analysis of a fan blade using unstructured dynamic meshesVAHDATI, M; IMREGUN, M.Proceedings of the Institution of Mechanical Engineers. Part C. Mechanical engineering science. 1996, Vol 210, Num 6, pp 549-564, issn 0263-7154Article

Vibration analysis of Mistuned bladed-disk assemblies : inverse approachSANLITURK, K. Y; IMREGUN, M.AIAA journal. 1994, Vol 32, Num 4, pp 857-865, issn 0001-1452Article

Fatigue life prediction using frequency response functionsSANLITURK, K. Y; IMREGUN, M.Journal of vibration and acoustics. 1992, Vol 114, Num 3, pp 381-386, issn 1048-9002Article

Structural damage detection using artificial neural networks and measured FRF data reduced via principal component projectionZANG, C; IMREGUN, M.Journal of sound and vibration. 2001, Vol 242, Num 5, pp 813-827, issn 0022-460XArticle

A survey of blade tip-timing measurement techniques for turbomachinery vibrationHEATH, S; IMREGUN, M.Journal of engineering for gas turbines and power. 1998, Vol 120, Num 4, pp 784-791, issn 0742-4795Conference Paper

Multi-stage beam modelling of turbomachinery bladesIMREGUN, M; VISSER, W. J.Finite elements in analysis and design. 1991, Vol 10, Num 1, pp 41-57, issn 0168-874XArticle

Numerical derivation of FRF matrices for curved, twisted and rotating beamsIMREGUN, M; TSOUTRELIS, A.Proceedings of the Institution of Mechanical Engineers. Part C. Mechanical engineering science. 1989, Vol 203, Num 6, pp 393-401, issn 0263-7154Article

Vibration modes of packeted bladed disksEWINS, D. J; IMREGUN, M.Journal of vibration, acoustics, stress, and reliability in design. 1984, Vol 106, Num 2, pp 175-180, issn 0739-3717Article

Semi-structured meshes for axial turbomachinery bladesSBARDELLA, L; SAYMA, A. I; IMREGUN, M et al.International journal for numerical methods in fluids. 2000, Vol 32, Num 5, pp 569-584, issn 0271-2091Article

Multi-bladerow fan forced response predictions using an integrated three-dimensional time-domain aeroelasticity modelSAYMA, A. I; VAHDATI, M; IMREGUN, M et al.Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science. 2000, Vol 214, Num 12, pp 1467-1483, issn 0954-4062Article

Thermoelastic Modeling of Rotor Response With Shaft RubZIAEI-RAD, S; KOUCHAKI, E; IMREGUN, M et al.Journal of applied mechanics. 2010, Vol 77, Num 6, issn 0021-8936, 061010.1-061010.12Article

Structural health monitoring and damage assessment using frequency response correlation criteriaZANG, C; FRISWELL, M. I; IMREGUN, M et al.Journal of engineering mechanics. 2007, Vol 133, Num 9, pp 981-993, issn 0733-9399, 13 p.Article

Frequency-domain criteria for correlating and updating dynamic finite element modelsZANG, C; GRAFE, H; IMREGUN, M et al.Mechanical systems and signal processing. 2001, Vol 15, Num 1, pp 139-155, issn 0888-3270Article

An integrated nonlinear approach for turbomachinery forced response prediction. Part II : Case studiesVAHDATI, M; SAYMA, A. I; IMREGUN, M et al.Journal of fluids and structures. 2000, Vol 14, Num 1, pp 103-125, issn 0889-9746Article

Parameters Identification for Nonlinear Dynamic Systems Via Genetic Algorithm OptimizationGONDHALEKAR, A. C; PETROV, E. P; IMREGUN, M et al.Journal of computational and nonlinear dynamics. 2009, Vol 4, Num 4, issn 1555-1415, 041002.1-041002.9Article

An integrated time-domain aeroelasticity model for the prediction of fan forced response due to inlet distortionBREARD, C; VAHDATI, M; SAYMA, A. I et al.Journal of engineering for gas turbines and power. 2002, Vol 124, Num 1, pp 196-208, issn 0742-4795Article

Forced response predictions for a HP turbine rotor bladeVAHDATI, M; GREEN, J; MARSHALL, J. G et al.RTO Meeting proceedings. 1999, pp 34.1-34.11, isbn 92-837-0005-8Conference Paper

On the use of atmospheric boundary conditions for axial-flow compressor stall simulationsVAHDATI, M; SAYMA, A. I; FREEMAN, C et al.Journal of turbomachinery. 2005, Vol 127, Num 2, pp 349-351, issn 0889-504X, 3 p.Article