B. Ghadiri

发表

Limit cycle oscillations of rectangular cantilever wings containing cubic nonlinearity in an incompressible flow

Mani Razi, M. Razi, B. Ghadiri, 2007 .

Aeroelastic response of a swept wing with cubic structural non-linearities

M. Razi, B. Ghadiri, M Razi, 2008 .

Numerical study of aeroelastic instability behavior of Nasa 37 transonic compressor rotor blades

B. Ghadiri, G. Heidarinejad, S. Fallah, 2017 .

NUMERICAL INVESTIGATION OF AIRFOIL GEOMETRIC VARIATIONS IMPACTS ON FLOW STRUCTURES IN A SUBSONIC FAN USING LARGE EDDY SIMULATION METHOD

B. Ghadiri, Mahmood Asgari Savadjani, 2018 .

Continuous-time state-space unsteady aerodynamic modeling based on boundary element method

Roeland De Breuker, Mostafa Abdalla, Hassan Haddadpour, 2012 .

NONLINEAR AEROELASTIC ANALYSIS OF SWEPT WINGS IN COMPRESSIBLE FLOW VIA THE HARMONIC BALANCE METHOD

M. Razi, B. Ghadiri, M. Mohammadi-Amin, 2012 .

CALCULATION OF LIMIT CYCLE OSCILLATION AMPLITUDE AND FREQUENCY OF AIRFOILS CONTAINING CUBIC NONLINEARITY

M. Razi, B. Ghadiri, 2011 .

DETERMINATION OF DYNAMIC INSTABILITY SPEED OF AN UNSWEEP WING IN SUBSONIC FLOW INCLUDING COMPRESSIBILITY EFFECTS

B. Ghadiri, R. G. Asl, 2007 .

Vibration Analysis of Elastic Uniform Cantilever Rotor Blades in Unsteady Aerodynamics Modeling

Mir Y. Ziabari, Behzad Ghadiri, B. Ghadiri, 2010 .