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Corrugation at the Trailing Edge Enhances the Aerodynamic Performance of a Three-Dimensional Wing During Gliding Flight [PDF]

open access: yesBiomimetics
Dragonflies exhibit remarkable flight capabilities, and their wings feature corrugated structures that are distinct from conventional airfoils. This study investigates the aerodynamic effects of three corrugation parameters on gliding performance at a ...
Kaipeng Li   +3 more
doaj   +2 more sources

Acoustic Improvement of Stator–Rotor Interaction with Nonuniform Trailing Edge Blowing [PDF]

open access: yesApplied Sciences, 2018
The results of unsteady-flow simulations and experiments are discussed to investigate active noise-reduction effects on the stator–rotor interaction in a single-stage low-speed compressor with nonuniform trailing edge blowing.
Wenjie Wang, Peter J. Thomas
doaj   +3 more sources

Trailing-Edge Flap Control for Mitigating Rotor Power Fluctuations of a Large-Scale Offshore Floating Wind Turbine under the Turbulent Wind Condition [PDF]

open access: yesEntropy, 2018
A trailing-edge flap control strategy for mitigating rotor power fluctuations of a 5 MW offshore floating wind turbine is developed under turbulent wind inflow. The wind shear must be considered because of the large rotor diameter. The trailing-edge flap
Bofeng Xu   +5 more
doaj   +2 more sources

Influence of the camber trailing-edge wings on the motion performance of underwater gliders

open access: yesInternational Journal of Naval Architecture and Ocean Engineering, 2022
Wings are the main source of lift for Underwater Gliders (UGs) and play a decisive role in their motion performance. The wings of UGs are generally rectangular and symmetrical airfoils.
Yuhong Liu   +6 more
doaj   +1 more source

Optimal design of watt six-bar transmission mechanism for morphing trailing edge [PDF]

open access: yesE3S Web of Conferences, 2021
The morphing trailing edge could realize a continuous smooth deformation compared with conventional trailing edge, which effectively improves the aerodynamic performance.
Zhou Jin, Zhao Shiwei
doaj   +1 more source

Influence of blade trailing edge profile on unsteady pressure pulsations in a multistage centrifugal pump

open access: yesEnergy Science & Engineering, 2023
Changing the shape of the blade trailing edge profile of a centrifugal pump is one of the effective means to improve the internal unsteady flow and pressure pulsation of a centrifugal pump.
Bao‐Ling Cui   +4 more
doaj   +1 more source

Influence of Cutting Angle of Blade Trailing Edge on Unsteady Flow in a Centrifugal Pump Under Off-Design Conditions

open access: yesApplied Sciences, 2020
The parameters of blade trailing edge have an important influence on the performance of centrifugal pump and internal unstable flow. In this study, the influences of cutting angles of blade trailing edge on unstable pressure pulsation and unstable flow ...
Baoling Cui   +3 more
doaj   +1 more source

CFD Simulation of Centrifugal Pump with Different Impeller Blade Trailing Edges

open access: yesJournal of Marine Science and Engineering, 2023
The centrifugal pump is one of the most widely used types of power machinery in the field of ship and ocean engineering, and the shape of the impeller blade trailing edge has an important influence on their performance.
Hui Li   +5 more
doaj   +1 more source

Airside heat transfer and pressure drop of an aluminum heat exchanger having a new louver fin with leading edge extension

open access: yesJournal of Thermal Science and Technology, 2021
Conventional louver fins have an inherent problem of condensate drainage. In this study, a newly developed louver fin is introduced. The louver fin has an extension at leading edge.
Nae-Hyun KIM
doaj   +1 more source

Center Body Airfoil Design for Blended Wing Body Configuration [PDF]

open access: yesXibei Gongye Daxue Xuebao, 2018
To design the center-body airfoil of a blended wing body configuration, the aerodynamic effects of the symmetrical airfoil, trailing-edge reflexed airfoil, leading-edge loaded airfoil and leading-edge loaded plus trailing-edge reflexed airfoil are ...

doaj   +1 more source

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