KARYOTYPE ANALYSIS OF B-LYMPHOCYTES TRANSFORMED BY EPSTEIN-BARR VIRUS IN 21 PATIENTS WITH B CELL CHRONIC LYMPHOCYTIC LEUKEMIAVAHDATI M; GRAAFLAND H; EMBERGER JM et al.1983; HUMAN GENETICS; ISSN 0340-6717; DEU; DA. 1983; VOL. 63; NO 4; PP. 327-331; BIBL. 40 REF.Article

11;14 TRANSLOCATIONS IN LYMPHOPROLIFERATIVE DISORDERS. AN ANALYSIS OF THREE CASESVAHDATI M; GRAAFLAND H; EMBERGER JM et al.1983; ACTA HAEMATOLOGICA; ISSN 0001-5792; CHE; DA. 1983; VOL. 70; NO 2; PP. 130-133; BIBL. 16 REF.Article

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

A numerical strategy for modelling rotating stall in core compressorsVAHDATI, M.International journal for numerical methods in fluids. 2007, Vol 53, Num 8, pp 1381-1397, issn 0271-2091, 17 p.Conference Paper

Design and development of a low NO_x Coanda ejector burnerVAHDATI, M. M; O'NIONS, P.Journal of the Institute of Energy. 2000, Vol 73, Num 494, pp 12-17, issn 0144-2600Article

Permeate flux modeling of membrane distillation = Modélisation du flux de perméat en distillation membranaireBURGOYNE, A; VAHDATI, M. M.Filtration & separation. 1999, Vol 36, Num 1, pp 49-53, issn 0015-1882Article

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

Aeroelasticity analysis of an industrial gas turbine combustor using a simplified combustion modelBREARD, C; SAYMA, A. I; VAHDATI, M et al.Journal of fluids and structures. 2002, Vol 16, Num 8, pp 1111-1126, issn 0889-9746, 16 p.Article

Whole-assembly flutter analysis of a low-pressure turbine bladeSAYMA, A; VAHDATI, M; IMREGUN, M et al.Aeronautical Journal. 1998, Vol 102, Num 1018, pp 459-463, issn 0001-9240Article

FEM-FCT: combining unstructured grids with high resolutionLOHNER, R; MORGAN, K; VAHDATI, M et al.Communications in applied numerical methods. 1988, Vol 4, Num 6, pp 717-729, issn 0748-8025Article

Part speed flutter of transonic fansCHEW, J. W; HAMBY, R. J; MARSHALL, J. G et al.RTO Meeting proceedings. 1999, pp 26.1-26.10, isbn 92-837-0005-8Conference Paper

Genetic differentiation in four species of Apodemus from Southern Europe: A. sylvaticus, A. flavicollis, A. agrarius and A. mystacinus (Muridae, Rodentia)BRITTON-DAVIDIAN, J; VAHDATI, M; BENMEHDI, F et al.Zeitschrift für Säugetierkunde. 1991, Vol 56, Num 1, pp 25-33, issn 0044-3468Article

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

Aeroelasticity analysis of air-riding seals for aero-engine applicationsSAYMA, A. I; BREARD, C; VAHDATI, M et al.Journal of tribology. 2002, Vol 124, Num 3, pp 607-616, issn 0742-4787Article

A fully distributed unstructured Navier-Stokes solver for large-scale aeroelasticity computationsBARAKOS, G; VAHDATI, M; SAYMA, A. I et al.Aeronautical Journal. 2001, Vol 105, Num 1050, pp 419-426, issn 0001-9240Article

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

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

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

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

Etude du caryotype de 52 leucémies lymphoïdes chroniques B = Karyotype in 52 cases of B cell CLLVAHDATI, M; GRAAFLAND, H; EMBERGER, J. M et al.Nouvelle revue française d'hématologie. 1984, Vol 26, Num 3, pp 189-195, issn 0029-4810Article

Unsteady Flow and Aeroelasticity Behavior of Aeroengine Core Compressors During Rotating Stall and SurgeVAHDATI, M; SIMPSON, G; IMREGUN, M et al.Journal of turbomachinery. 2008, Vol 130, Num 3, issn 0889-504X, 031017.1-031017.9Article

An integrated nonlinear approach for turbomachinery forced response prediction. Part I : FormulationSAYMA, A. I; VAHDATI, M; IMREGUN, M et al.Journal of fluids and structures. 2000, Vol 14, Num 1, pp 87-101, issn 0889-9746Article

Improved process topology for membrane distillationFOSTER, P. J; BURGOYNE, A; VAHDATI, M. M et al.Separation and purification technology. 2001, Vol 21, Num 3, pp 205-217, issn 1383-5866Article

Multi-objective optimization of a solar-hybrid cogeneration cycle: Application to CGAM problemSOLTANI, R; MOHAMMADZADEH KELESHTERY, P; VAHDATI, M et al.Energy conversion and management. 2014, Vol 81, pp 60-71, issn 0196-8904, 12 p.Article

Multibladerow forced response modeling in axial-flow core compressorsVAHDATI, M; SAYMA, A. I; IMREGUN, M et al.Journal of turbomachinery. 2007, Vol 129, Num 2, pp 412-420, issn 0889-504X, 9 p.Article