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241
Drag Reduction On Naca 2412 Using Dimpled Airfoil And Grooved Wing
Published 2020“…The analyses of the dimpled airfoil and groove wing with different configurations showcased the sensitivity of flow over rough airfoil on pressure and suction side.…”
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Thesis -
242
Analysis And Comparison Of Airfoil-Polar Prediction Methods For Vertical-Axis Turbines
Published 2021“…Thus, full-range airfoil data is required to compute the turbine performance of VAT. …”
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Monograph -
243
Flow topology around low reynolds number airfoils with vortex shedding
Published 2020“…While the topology methodology is quite well established, the majority of airfoil types have still not been covered. In this study, six low Reynolds number airfoils were considered to investigate the separation bubble structure, vortex shedding and reattachment point. …”
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244
Wind tunnel test to investigate transition to turbulence on wind turbine airfoil
Published 2014“…The choice of the airfoils with excellent aerodynamics characteristics is an essential step in the design of wind turbine blade in order to obtain optimal performances. …”
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Thesis -
245
Design Optimization of a Multi-Megawatt Wind Turbine Blade with the NPU-MWA Airfoil Family
Published 2019-08-01Subjects: Get full text
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Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coanda Jet
Published 2013“…A trade-off study on the S809 Coanda configured airfoil is needed to judge the optimum configuration of Coandă-jet fitted Wind-Turbine design.…”
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252
Parametric investigation on the aerodynamic characteristic of NACA2415 airfoil at low reynolds number
Published 2013“…This study is to investigate the aerodynamic characteristic of an airfoil in low Reynolds number flow. NACA2415 airfoil is chosen as the test subject as it has been studied by many researches and documented. …”
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Undergraduates Project Papers -
253
Reduction in Airfoil Trailing-Edge Noise Using a Pulsed Laser as an Actuator
Published 2023-01-01“…Trailing-edge noise (TE noise) is an aeroacoustic sound radiated from an isolated airfoil in the specific ranges of low-speed flow. …”
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Article -
254
Numerical Study of the Influence of the Critical Reynolds Number on the Aerodynamic Characteristics of the Wing Airfoil
Published 2023-10-01“…The mechanism of the appearance and interaction of laminar and turbulent flow separation near the leading and trailing edges of the airfoil is studied in detail. In the paper, the dependence of aerodynamic forces on the critical Reynolds number for the HGR01 airfoil is discussed. …”
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255
Influence of the Blunt Trailing-Edge Thickness on the Aerodynamic Characteristics of the Very Thick Airfoil
Published 2023-10-01Subjects: “…very thick airfoil…”
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Article -
256
Aerodynamic Characteristics of Morphing Supercritical Airfoils for Aircraft with All-Stage High Performance
Published 2022-01-01Subjects: “…morphing supercritical airfoil…”
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257
Application of Simultaneous Symmetric and Cambered Airfoils in Novel Vertical Axis Wind Turbines
Published 2021-08-01Subjects: Get full text
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258
Shedding vortex characteristics analysis of NACA 0012 airfoil at low Reynolds numbers
Published 2022-07-01“…The rising section and falling section of airfoil lift and drag coefficient curves correspond to the vortex shedding and formation respectively. …”
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259
Experimental Study of Airfoil Leading Edge Combs for Turbulence Interaction Noise Reduction
Published 2020-04-01“…The most likely reasons for this frequency shift are that the teeth of the combs break up large incoming turbulent eddies into smaller ones or that they shift turbulent eddies away from the airfoil surface, thereby reducing pressure fluctuations acting on the airfoil. …”
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260
Flow Characteristics and Parameter Influence of the Under-Expansion Jet on Circulation Control Airfoil
Published 2023-04-01“…The enhancement in the jet pressure ratio and jet velocity contributes to expanding the control efficiency and control boundary of circulation control airfoil under high subsonic incoming flow. However, because of an excessive jet pressure ratio, the jet separates prematurely on the Coanda surface, resulting in control failure. …”
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Article