Upgraded Reduction Technique for Dynamic Analysis of Structures with Friction Contact von Mashayekhi, F, Zucca, S, Nobari, A. S

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Aeroelastic Stability of Hingeless Rotor Blades in Hover Using Fully Intrinsic Equations von Amoozgar, M. R, Shahverdi, H, Nobari, A. S

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Identification of dynamic characteristics of nonlinear joint based on the optimum equivalent linear frequency response function von Kashani, H., Nobari, A.S.

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Layer-wise dynamic analysis of a beam with global and local viscoelastic contributions using an FE/Laplace transform approach von Kiasat, Sh, Filippi, M., Nobari, A. S., Carrera, E.

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Identification of Dynamic (Young’s and Shear) Moduli of a Structural Adhesive Using Modal Based Direct Model Updating Method von Jahani, K., Nobari, A. S.

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Identification of the dynamic characteristics of a viscoelastic, nonlinear adhesive joint von Naraghi, T., Nobari, A.S.

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Aeroelastic analysis of helicopter rotor blade in hover using an efficient reduced-order aerodynamic model von Shahverdi, H., Nobari, A.S., Behbahani-Nejad, M., Haddadpour, H.

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Hybrid reduction of mistuned bladed disks for nonlinear forced response analysis with dry friction von Mashayekhi, F., Nobari, A.S., Zucca, S.

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Aeroelastic stability consideration of supersonic flight vehicle using nonlinear aerodynamic response surfaces von Fathi Jegarkandi, M., Nobari, A.S., Sabzehparvar, M., Haddadpour, H.

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Study of surface bonding imperfection effects on equivalent identified dynamic Young’s and shear moduli using a modal based joint identification method von Meshki, M.M., Nobari, A.S., Nikbin, K.

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Identification of mechanical properties of adhesive joints using ANN von Pazand, Kamran, Nobari, A S

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An efficient reduced-order modelling approach based on fluid eigenmodes and boundary element method von Shahverdi, H., Nobari, A.S., Behbahani-Nejad, M., Haddadpour, H.

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Plate vibration suppression by optimizing friction threshold at its bolted supports von Hallajisani, Sara, Kashani, Hamed, Nobari, A. S.

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Nonlinear aeroelastic stability analysis of hingeless helicopter rotor blades using FRF coupling and condition number von Roknizadeh, S. A. S., Nobari, A. S., Shahverdi, H.

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A new frequency domain based approach for a nonlinear aeroelasticity analysis von S. Roknizadeh, S.A., Nobari, A.S., Shahverdi, H.

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Structural Nonlinearity Identification Using Perturbed Eigen Problem and ITD Modal Analysis Method von Kashani, H., Nobari, A.S.

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Characterization of viscoelastic damping mechanism in a delaminated structure von Kiasat, Sh, Nobari, A.S., Filippi, M., Carrera, E.

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Identification of Damping Characteristic of a Structural Adhesive by Extended Modal Based Direct Model Updating Method von Nobari, A. S., Jahani, K.

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Identification of a nonlinear joint in an elastic structure using optimum equivalent linear frequency response function von Sadati, S. M. Sajed, Nobari, A. S., Naraghi, Tahereh

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Improvement of Nonlinear Single Resonant Mode Method von Nobari, A. S, Shahramyar, M

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