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181
A study of aerodynamic sound generated from an airfoil placed in a flow with turbulence (2nd Report: In the case of airfoil subjected to circular-cylinder wake)
Published 2020-04-01“…The wind velocity is set to 30 m/s, which results in an airfoil Reynolds number of 3.0×105. The circular cylinder is set 100 mm upstream of the leading edge of the airfoil, and its diameter as well as installation position in the transverse direction are varied. …”
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182
Airfoil Shape Morphing through a Novel Parameterization and Fitting Optimization Method Based on Uniform Non-Rational B-Spline Functions
Published 2023-02-01Subjects: “…airfoil optimization…”
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183
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186
Gradient-Based Aerodynamic Optimization of an Airfoil with Morphing Leading and Trailing Edges
Published 2021-02-01“…This article presents a gradient-based aerodynamic optimization framework and investigates optimum deformations for a transonic airfoil equipped with morphing leading and trailing edges. …”
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187
Lightweight design of piezoelectric linear displacement accumulation actuator for airfoil deployment
Published 2023-10-01Get full text
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188
Aerodynamic Shape Optimisation of a Camber Morphing Airfoil and Noise Estimation
Published 2022-01-01“…In order to decrease the emitted airframe noise by a two-dimensional high-lift configuration during take-off and landing performance, a morphing airfoil has been designed through a shape design optimisation procedure starting from a baseline airfoil (NLR 7301), with the aim of emulating a high-lift configuration in terms of aerodynamic performance. …”
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189
Model Identifying the Airfoilicing Process Beginning on the Basis of Aircraft Flight Parameters
Published 2022-01-01Get full text
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190
Optimizing NACA2414 airfoil aerodynamics with PARSEC parametrization and Genetic Algorithm
Published 2024-01-01“…This research endeavours to contribute to the broader field of wind turbine aerodynamics by investigating a method to enhance the performance of airfoils, with specific attention to the NACA2414 airfoil at a 15-degree angle of attack. …”
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191
Numerical solution of unsteady flow on airfoils with vibrating local flexible membrane
Published 2016-01-01“…Unsteady flow separation on the airfoils with local flexible membrane (LFM) has been investigated in transient and laminar flows by the finite volume element method. …”
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192
Numerical Simulation of Roughness Effects of Ice Accretion on Wind Turbine Airfoils
Published 2022-11-01“…The RWFs are used to simulate airflow field over the airfoil profiles with ice profile attached to its leading edge using OpenFOAM CFD framework. …”
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193
Optimizing Airfoil Aerodynamic Characteristics by Using Proposed CSA-KJ Method
Published 2023-01-01Subjects: Get full text
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194
Quasisolutions of Inverse Boundary-Value Problem of Aerodynamics for Dense Airfoil Grids
Published 2016-12-01Subjects: Get full text
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195
Experimental and Numerical Icing Penalties of an S826 Airfoil at Low Reynolds Numbers
Published 2020-04-01Subjects: Get full text
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196
Analysis of Flow Characteristic of Transonic Tandem Rotor Airfoil and Its Optimization
Published 2020-08-01Subjects: “…prescribed velocity distribution airfoil…”
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197
Scour Reduction around Bridge Pier Using the Airfoil-Shaped Collar
Published 2023-03-01Subjects: Get full text
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198
On the Accuracy of Numerical Schemes for Flow Simulation Around Airfoils with Angle Point
Published 2015-01-01“…The aim of this research is to investigate the accuracy of the numerical schemes of VEM, which use different approaches to satisfy boundary conditions on the surface of airfoil in case of simulation of the flow around airfoils with angle point.…”
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199
Numerical Study of Aerodynamic Performance of Airfoil with Variable Curvature Split Flap
Published 2023-03-01“…The lift-type vertical axis wind turbine's typical blade airfoil NACA 0018 is taken as the research object. …”
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200
Active Flow Control of a Supercritical Airfoil and Flap with Sweeping Jets
Published 2023-09-01“…An experimental study on the AFC of flaps, using sweeping jets, was carried out using a NASA SC(2)-0410 supercritical airfoil wind-tunnel model at <i>Re</i> = 2.0 × 10<sup>5</sup> (with velocity <i>V</i> = 10 m/s). …”
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