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| # | Type | Title | Author | Publisher | Pub. Year | Subjects | Call Number |
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| 1 | مقاله | Association Between Gait Deviation Index and Rodda's Levels of Gait Severity in Children with Cerebral Palsy | Davari, M. M. | 2024 |
Cerebral Palsy.
Gait Analysis. GDI. Rodda Classification. Brain. Damage detection. Gait analysis. Brain damage. Cerebral palsy. Children with cerebral palsies. Equinus. Gait deviation index. Gait pattern. Kinematics parameters. Reliable methods. Rodda classification. Diseases. |
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| 2 | مقاله | The unsteady behavior of subsonic wind tunnel wall pressure during pitching motion of the model | Davari, A. R. | 2014 |
Disturbance convection.
Interference effect. Experiments. Interference suppression. Reynolds number. Low-speed wind tunnel. Oscillation parameters. Pitching oscillation. Reduced frequency. Subsonic wind tunnels. Unsteady behaviors. Wall-pressure distribution. Flow modeling. Oscillating flow. Parameterization. Streamflow. Wind tunnel. |
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| 3 | مقاله | On the relationship between unsteady forces and shock angles on a pitching airplane model | Davari, A. R. | 2010 |
Pitching motion.
Reduced frequency. Schlieren. Upstroke. Vortex bursting. Aerodynamic forces. After-images. Angles of attack. Normal forces. Oscillation cycles. Oscillation frequency. Shock angle. Static and dynamic. Angle of attack. Flight dynamics. Hysteresis loops. Magnetic materials. Aerodynamics. Aircraft. Hysteresis. Mage processing. Numerical model. Visualization. Vortex. Wave action. |
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| 4 | مقاله | Cosmological constrains on minimally and non-minimally coupled scalar field models | Davari, Z. | Oxford University Press, | 2020 |
Cosmology: theory.
Dark energy. Methods: analytical. |
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| 5 | مقاله | Effects of plunging motion on unsteady aerodynamic behavior of an aircraft model in compressible flow | Davari, A. R. | 2007 |
Aerodynamics.
Aircraft. Compressible flow. Flow fields. Mach number. Mathematical models. Unsteady flow. Hysteresis. Wind tunnel. |
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| 6 | مقاله | On wind tunnel wall pressure fluctuations during an unsteady test of a fighter model | Davari, A. R. | 2005 |
Angles of attack.
Dynamics modeling. Free stream mach numbers. Modeling motions. Oscillation amplitude. Reduced frequency. Time variations. Wind tunnel walls. Aircraft models. Angle of attack. Fluid dynamics. Identification (control systems) Wind tunnels. Pressure effects. |
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| 7 | مقاله | Force and moment measurements on a fighter model in heaving motion | Davari, A. R. | American Institute of Aeronautics and Astronautics Inc, | 2005 |
Aerodynamics.
Force control. Missiles. Natural frequencies. Oscillations. Fighter models. Heaving motion. Moment measurements. Fighter aircraft. |
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| 8 | مقاله | An experimental investigation of transition point over a quasi-2D swept wing by using hot film | Hassanzadeh Khakmardani, M. | SAGE Publications Ltd, | 2015 |
Boundary layer.
Hot-film sensor. Aspect ratio. Laminar flow. Reynolds number. Transition flow. Angles of attack. Experimental investigations. Flow instabilities. Instability modes. Low Reynolds number. Transition. Transition locations. Swept wings. |
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| 9 | مقاله | Statistical analysis on the effect of reduced frequency on the aerodynamic behavior of an airfoil in dynamic physical motions | Razavi Dehkordi, M. H. | Elsevier B.V, | 2019 |
Combined pitch–plunge motions.
Pressure distribution. Pure pitch oscillation. Reduced frequency. Statistical analysis. Airfoils. Lift. Pressure distribution. Reynolds number. Statistical methods. Aerodynamic characteristics. Angles of attack. Experimental test. Modeling motions. Pitch oscillations. Reduced frequency. Surface pressure distribution. Vertical displacements. Angle of attack. |
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| 10 | مقاله | Experimental investigation of aerodynamic performance of a wind turbine blade undergoing pure pitch and plunge motions | Razavi Dehkordi, M. H. | Penerbit Akademia Baru, | 2020 |
Lift.
Moment. Pitch oscillation. Plunge oscillation. Pressure distribution. Reduced frequency. |
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| 11 | مقاله | Experimental investigation of slip velocity and settling distribution of micro-particles in converging–diverging microchannel | Shirinzadeh, F. | Springer Verlag, | 2016 |
Domain walls.
Microchannels. Reynolds number. Diverging microchannels. Experimental investigations. Experimental testbed. Low Reynolds number. Sedimentation of particles. Single particle tracking. Three-dimensional velocity. Velocity of particles. Velocity. |
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| 12 | مقاله | Experimental investigation of slip velocity and settling distribution of micro-particles in converging–diverging microchannel | Shirinzadeh, F. | Springer Verlag, | 2017 |
Domain walls.
Microchannels. Reynolds number. Diverging microchannels. Experimental investigations. Experimental testbed. Low Reynolds number. Sedimentation of particles. Single particle tracking. Three-dimensional velocity. Velocity of particles. Velocity. |
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| 13 | مقاله | Optical drive of amplitude and phase modes in excitonic insulators | Davari, E. | ACS Journal, | 2024 |
Electron correlations.
Electron-phonon interactions. Energy gap. Ground state. Narrow band gap semiconductors. Optical lattices. Polarization. Semiconductor lasers. Transition metals. Dichalcogenides. Electron phonon couplings. Excitonic condensate. Excitonic insulator. Laser fields. Laser light beams. Layered chalcogenides. Optical drive. Dynamics. |
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| 14 | مقاله | Canard flow improvement in a split canard configuration | Davari, A. R. | 2015 |
Canard.
Delta wing. Downwash. Leading edge vortex. Angle of attack. Vortex flow. Wakes. Wind tunnels. Delta wings. Flow field structure. High angles of attack. Leading-edge vortices. Low-speed wind tunnel. Performance enhancements. Delta wing aircraft. |
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| 15 | مقاله | Neural network: A new prediction tool for estimating the aerodynamic behaivior of a pitching delta wing | Soltani, M. R. | American Institute of Aeronautics and Astronautics Inc, | 2003 |
Aerodynamics.
Wind tunnels. Swept wings. Neural networks. Forecasting. |
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| 16 | مقاله | A new method for predicting the amplitude and frequency of a highly swept wing undergoing rocking motion | Soltani, M. R. | Sharif University of Technology, | 2003 |
Wing.
Oscillation. Aerodynamics. |
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| 17 | مقاله | A simple analytical method for predicting the amplitude and frequency of a delta wing model undergoing rocking motion | Soltani, M. R. | American Institute of Aeronautics and Astronautics Inc, | 2002 |
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| 18 | مقاله | Effects of canard position on wing surface pressure | Soltani, M. R. | 2010 |
Canard.
Delta wing. Downwash. Leading edge vortex. Angles of attack. Canard configuration. Delta wings. High angles of attack. Leading-edge vortices. Position effect. Various configuration. Vertical positions. Wind tunnel tests. Wing surface. Delta wing aircraft. Fighter aircraft. Flow fields. Wakes. Angle of attack. Experimental study. Flow field. Surface pressure. Vortex. Wind field. Wind tunnel. |
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| 19 | مقاله | Effects of wing geometry on wing-body-tail interference in subsonic flow | Davari, A. R. | 2011 |
Forebody vortex shedding.
Interference. Tip vortex. A-plane. Flow direction. Geometric parameter. Interference effects. Span ratios. Surface pressure distribution. Sweep wings. Velocity contours. Wind tunnel tests. Wing aspect ratio. Wing geometry. Wingtip vortex. Aerodynamics. Aspect ratio. Flow fields. Vortex flow. Wind tunnels. Subsonic flow. Flow field. Geometry. Vortex. Wind tunnel. |
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| 20 | مقاله | Vibration of rotating functionally graded timoshenko nano-beams with nonlinear thermal distribution | Azimi, M. | Taylor and Francis Inc, | 2018 |
Cantilever boundary condition.
Rotating nano-beam. Boundary conditions. Differentiation (calculus) Elasticity. Nanocantilevers. Thermal effects. Thermal stress. Differential quadrature methods. Governing equations. Hamilton's principle. Nano beams. Non-local elasticity theories. Temperature dependent. Thermal distributions. Timoshenko model. Vibration analysis. |
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