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Experimental study of the effects of a vertical channel on the natural convection of a horizontal cylinder
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10.2298/TSCI190630091A |
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Effect of nature-inspired needle-shaped vortex generators on the aerodynamic features of a double-delta wing
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10.1016/j.ijmecsci.2021.106502 |
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Aerodynamic Inverse Design of Transonic Compressor Cascades with Stabilizing Elastic Surface Algorithm
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10.3390/app11114845 |
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Inverse shape design method based on pressure and shear stress for separated flow via Elastic Surface Algorithm
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10.1080/17415977.2021.1914604 |
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Experimental study of flow structures of a solitary wave over two rectangular tandem obstacles
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10.1007/s40430-021-02944-3 |
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Inverse design of 3D curved ducts using a 3D-upgraded ball-spine algorithm
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10.1080/17415977.2021.1894143 |
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Full Three-Dimensional Inverse Design Method for S-Ducts Using a New Dimensionless Flow Parameter
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10.3390/app11031119 |
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Design of an axial transonic rotor by modified span-wise loading distribution
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A novel self-seeding method for particle image velocimetry measurements of subsonic and supersonic flows
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10.1038/s41598-020-67680-5 |
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Design of a novel vortex-based feedback fluidic oscillator with numerical evaluation
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10.1080/19942060.2020.1826360 |
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Effects of elasticity on unsteady forced convective heat transfer of viscoelastic fluid around a cylinder in the presence of viscous dissipation
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10.1063/5.0009948 |
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Evaluation of aerodynamic performance enhancement of Ris?_B1 airfoil with an optimized cavity by PIV measurement
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A novel approach for the design of axial flow fan by increasing by-pass ratio in a constant-diameter turbofan
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10.1016/j.jppr.2020.04.005 |
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VORTEX-INDUCED VIBRATION CHARACTERISTICS AND HEAT TRANSFER MECHANISM OF AN OSCILLATING PLATE ATTACHED TO A CYLINDER IN A CONSTANT-TEMPERATURE CHANNEL
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10.1615/HeatTransRes.2019030374 |
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Forced convective heat transfer of nonlinear viscoelastic flows over a circular cylinder at low Reynolds inertia regime
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10.1016/j.cnsns.2019.105134 |
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The influence of cubic real-gas equations of state in the supersonic regime of dense gases
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10.1007/s12206-020-0320-3 |
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طراحي معكوس كسكيد پره كمپرسور محوري در جريان غير لزج مادون صوت با استفاده از روش پوسته الاستيك ارتقاءيافته
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An experimental study on the effect of a novel nature-inspired 3D-serrated leading edge on the aerodynamic performance of a double delta wing in the transitional flow regime
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