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Experimental study of riblet effects on the aerodynamic performance and flow characteristics of a delta wing
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10.1177/0954410017748989 |
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Numerical study of camber and stagger angle effects on the aerodynamic performance of tandem-blade cascades
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Experimental Study of Flow Structures of a Solitary Wave Propagating over a Submerged Thin Plate in Different Angles using PIV Technique
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Investigation of an innovative non-free vortex aerodynamic procedure to design a single-stage transonic compressor
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10.1177/0954410017710272 |
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Experimental Study of Natural Convective Flow over a Hot Horizontal Rhombus Cylinder Immersed in Water via PIV Technique
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Flow visualization over a thick blunt trailing-edge airfoil with base cavity at low Reynolds numbers using PIV technique
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10.1007/s12650-016-0405-3 |
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Improvement of ventilation and heat transfer in Shavadoon via numerical simulation A traditional HVAC system
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Determination of desired geometry by a novel extension of ball spine algorithm inverse method to conjugate heat transfer problems
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Performance Improvement of a Wind Turbine Blade using a Developed Inverse Design Method
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Aerodynamic performance of a circulating airfoil section for Magnus systems via numerical simulation and flow visualization
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Optimization of a subsonic wind tunnel nozzle with low contraction ratio via ball-spine inverse design method
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Numerical analysis of turbocharger s bearing using dynamic mesh
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Development of the ball-spine inverse design algorithm to swirling viscous flow for performance improvement of an axisymmetric bend duct
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Inverse shape design for heat conduction problems via the ball spine algorithm
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10.1080/10407790.2015.1096690 |
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Three-Dimensional Design of Axial Flow Compressor Blades Using the Ball-Spine Algorithm
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Aerodynamic Design of S-Shaped Diffusers Using Ball Spine Inverse Design Method
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Applying the ball-spine algorithm to the design of blunt leading edge airfoils for axial flow compressors
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Inverse design in subsonic and transonic external flow regimes using Elastic Surface Algorithm
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A Novel Strategy for Designing and Manufacturing a Fixed Wing MAV for the Purpose of Increasing Maneuverability and Stability in Longitudinal Axis
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A Novel aerodynamic Design Method for Centrifugal Compressor Impeller
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