Article
Thermodynamics
Chengyong Zhu, Yingning Qiu, Tongguang Wang
Summary: This paper presents comparative analyses of dynamic stall among the 2D airfoil, 3D non-rotating blade and 3D rotating blade undergoing sinusoidal pitch oscillations, with a focus on the impact of rotational augmentation on dynamic stall. The study found that rotational augmentation can effectively delay the onset of dynamic stall, increase the maximum lift coefficient, and significantly reduce the aerodynamic hysteresis intensity.
Article
Engineering, Marine
Qing Wang, Muyao Yu, Deshun Li, Rennian Li
Summary: This study investigates the dynamic stall of the S809 airfoil under a sand-wind environment, which has rarely been considered in previous studies. The simulations reveal that sand particles with a diameter of 10 μm decrease the maximum lift coefficient and drag coefficient by approximately 2.18% and 2.52% respectively compared to clear air. Moreover, a particle concentration of 62.6 g/m3 results in a 6.93% decrease in the maximum lift coefficient. The results also indicate that the decrease in lift and drag coefficients becomes more significant with higher particle concentrations, suggesting reduced efficiency of wind turbines in sand storm weather.
Article
Green & Sustainable Science & Technology
D. De Tavernier, C. Ferreira, A. Vire, B. LeBlanc, S. Bernardy
Summary: The study demonstrates that vortex generators (VGs) can delay or suppress dynamic stall process in unsteady flow conditions, with important factors being VG height and mounting position. Configurations with VGs show a larger loss in normal coefficient when VG effectiveness vanishes, but the flow reattaches quicker and the airfoil recovers easier from deep-stall conditions.
Article
Engineering, Mechanical
Zhen Chen, Zhiwei Shi, Sinuo Chen, Zhangyi Yao
Summary: This article investigates the effect of leading-edge blowing on the suppression of stall flutter. It is found that leading-edge blowing can change the bifurcation behavior of flutter, reducing the flutter amplitude and increasing the flutter critical velocity. Measurements of dynamic response and observation of flowfield evolution demonstrate that leading-edge blowing effectively controls dynamic stall and promotes the decay of flutter.
JOURNAL OF FLUIDS AND STRUCTURES
(2022)
Article
Engineering, Marine
Ahmed Aboelezz, Hani Ghali, Gamal Elbayomi, Mohamed Madboli
Summary: This paper introduces the application of a guided vane airfoil to control the dynamic stall of a Darrieus vertical axis wind turbine. Numerical simulations and experimental tests are conducted to investigate the effect of the guided vane on the aerodynamics performance of the NACA 0018 airfoil. The results show that the guided vane significantly improves the power output of the wind turbine.
Article
Multidisciplinary Sciences
Galih Bangga, Surya Hutani, Henidya Heramarwan
Summary: Increasing airfoil thickness is found to be beneficial in suppressing dynamic stall effects and improving the performance of high solidity turbines, despite a slight reduction in thrust component. The strength and radius of the dynamic stall vortex decrease with increasing airfoil thickness, which strongly influences the pressure distributions during the dynamic stall process.
ADVANCED THEORY AND SIMULATIONS
(2021)
Article
Automation & Control Systems
He-sen Yang, Hua Liang, Guang-yin Zhao
Summary: The study explored the application of nanosecond dielectric barrier discharge technology in controlling dynamic stall and identified key findings through experiments and measurements: control of stall requires actuation voltage above a threshold, high F(+) maintains peak lift, and control effectiveness decreases with increasing reduced frequencies.
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING
(2021)
Article
Green & Sustainable Science & Technology
Yosra Chakroun, Galih Bangga
Summary: This study investigates the effects of Gurney flaps on aerodynamic characteristics of an airfoil and a vertical axis wind turbine. The results show that using Gurney flaps increases lift coefficient and power production. Additionally, increasing flap height improves turbine performance.
Article
Energy & Fuels
Francesco Papi, Alberto Nocentini, Giovanni Ferrara, Alessandro Bianchini
Summary: This study aims to provide a comprehensive annotated procedure for the full preliminary design process of a new SWT, focusing on combining modern engineering methods and codes. Results show that proper aerodynamic optimization coupled with pitch-to-feather regulation can increase annual energy production by over 12% compared to a conventional approach.
Article
Energy & Fuels
Galih Bangga, Steven Parkinson, William Collier
Summary: Considering the dynamic stall effects is crucial for accurate engineering calculations of wind turbine aerodynamic loads, which greatly impact turbine aeroelastic stability during power production and stand-still cases. The recently implemented IAG dynamic stall model in Bladed, transformed into a state-space representation, is validated against measurement data and other dynamic stall models for various airfoils and flow conditions. Results show that the new model accurately reproduces the measured dynamic polar without airfoil specific parameter calibration, outperforming the incompressible Beddoes-Leishman model and the oye model in Bladed.
Article
Engineering, Marine
Junwei Yang, Hua Yang, Xiangjun Wang, Nailu Li
Summary: The present work aimed to investigate the aerodynamic characteristics of a pitching wind turbine airfoil with a Gurney flap under turbulent inflow. Experimental results showed that with increased turbulence intensity, the differences in lift hysteresis loops between the baseline airfoil and flapped airfoil became smaller. The Gurney flap was found to be more stable in turbulent conditions compared to the baseline airfoil.
JOURNAL OF MARINE SCIENCE AND ENGINEERING
(2022)
Article
Thermodynamics
Chengyong Zhu, Yingning Qiu, Yanhui Feng, Tongguang Wang, Hui Li
Summary: Dynamic stall on wind turbines causes highly unsteady and nonlinear aerodynamic loads. This study investigates the combined effect of passive vortex generators (VGs) and leading-edge roughness (LER) on dynamic stall of the NREL S809 airfoil. Results show that LER accelerates separated flow and dynamic stall onset, while VGs delay dynamic stall and reduce aerodynamic hysteresis. Additionally, double-row VGs outperform single-row VGs in improving aerodynamic performance of roughened airfoils.
ENERGY CONVERSION AND MANAGEMENT
(2022)
Article
Energy & Fuels
Florian N. Schmidt, Jochen Wild
Summary: This article describes the development of a passive-adaptive slat for a wind turbine blade, which delays stall angle and increases lift to drag ratio. The experimental results show an improved aerodynamic performance compared to fixed slats.
Article
Engineering, Mechanical
Junwei Yang, Hua Yang, Xiangjun Wang
Summary: This study aims to extend and modify the L-B model to predict the unsteady aerodynamic characteristics of a wind turbine airfoil equipped with a Gurney flap. A prediction module was proposed based on the unsteady aerodynamic changes of the Gurney flap and the characteristics of vortex generation and shedding traveling on the airfoil surface. The results were preliminarily confirmed through a wind tunnel experiment, indicating the high practical potential of this approach.
ACTA MECHANICA SINICA
(2023)
Article
Energy & Fuels
Deshun Li, Ting He, Qing Wang
Summary: This paper investigates the impact of particle parameters on the airfoil dynamic stall through numerical simulation. The study reveals that the addition of particles reduces the aerodynamic performance of the airfoil, especially at large angles of attack. Moreover, the larger the particle diameter, the larger the vortex volume near the airfoil's leading edge, and a significant amount of particles gather at the suction surface of the airfoil. Additionally, as the particle concentration increases, the separation point of the airfoil occurs earlier and the erosion rate of the airfoil increases.
Article
Engineering, Civil
Yihua Peng, Ramsankar Veerakumar, Yang Liu, Xuhui He, Hui Hu
JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS
(2020)
Article
Engineering, Aerospace
Cem Kolbakir, Haiyang Hu, Yang Liu, Hui Hu
AEROSPACE SCIENCE AND TECHNOLOGY
(2020)
Article
Engineering, Environmental
Zichen Zhang, Liqun Ma, Yang Liu, Juan Ren, Hui Hu
Summary: The experimental investigation evaluated the variations of surface wettability and ice adhesion strength on a hydro-/ice-phobic surface under continuous impingement of water droplets at relatively high speeds, using a specially designed rain erosion testing rig. Surface rheological properties and ice adhesion strength were quantified, and surface topology changes were measured using an Atomic Force Microscope system. The correlation between surface characteristics and rain erosion effects was studied for a better understanding of hydro-/ice-phobic coatings in the context of UAS inflight icing mitigation.
COLD REGIONS SCIENCE AND TECHNOLOGY
(2021)
Article
Green & Sustainable Science & Technology
Liqun Ma, Zichen Zhang, Linyue Gao, Hui Hu
Article
Engineering, Aerospace
Vishal Raul, Leifur Leifsson
Summary: The dynamic stall phenomenon is characterized by the formation of a leading-edge vortex, which impacts the structural strength and life of a system. Aerodynamic shape optimization provides a cost-effective method to delay or mitigate these characteristics, but it requires time-consuming CFD simulations. A surrogate-based optimization technique is proposed in this work to reduce the computational cost of ASO for airfoil dynamic stall characteristics.
AEROSPACE SCIENCE AND TECHNOLOGY
(2021)
Article
Green & Sustainable Science & Technology
Linyue Gao, Tao Tao, Yongqian Liu, Hui Hu
Summary: Study examined ice accretion on 50m-long turbine blades and icing-induced power production losses. Found more ice on outboard blades, up to 0.3m thick near blade tips. Theoretical predictions matched field measurements well. Turbines rotated slower and shut down frequently during icing event, with up to 80% power loss. Aimed to bridge gap between lab studies and real-world icing phenomena.
Article
Computer Science, Interdisciplinary Applications
Vishal Raul, Leifur Leifsson
Summary: The research shows that varying the trust-region radius significantly affects the prediction accuracy of the MFM. The HF and LF simulation models hold similarity within small to medium TR radii producing a prediction error less than 5%, while large TR radii are strongly affected by time discretization and minimally by spatial discretization. The findings provide new insights for constructing accurate MFMs in dynamic stall performance prediction using LF model spatial and temporal discretization setup and TR radius size.
ENGINEERING COMPUTATIONS
(2022)
Article
Thermodynamics
Kuan Zheng, Wei Tian, Jiang Qin, Hui Hu
Summary: This study demonstrates that placing a micro-vortex generator upstream of the cooling hole can enhance film cooling performance, particularly at high blowing ratios. The upstream VG counteracts the detrimental effects of the coolant jet, leading to extended coverage of cooling gas in the spanwise direction.
EXPERIMENTAL THERMAL AND FLUID SCIENCE
(2021)
Article
Mechanics
Kai Zhang, Hui Hu
Summary: The experimental study revealed the dynamic runback process of wind-driven water film/rivulet flows under various conditions, including the formation of surface waves, the motion patterns of rivulets, and the merging of rivulet flows.
Article
Thermodynamics
Yihua Peng, Ramsankar Veerakumar, Zichen Zhang, Haiyang Hu, Yang Liu, Xuhui He, Hui Hu
Summary: The experimental study showed that utilizing a superhydrophobic surface coating on bridge cables can significantly reduce ice coverage and mass, as well as decrease aerodynamic drag forces. However, the effectiveness of the SHS coating in ice mitigation was found to be less effective under rime icing conditions, but it can reduce aerodynamic drag forces at the initial stage of the rime icing process.
EXPERIMENTAL THERMAL AND FLUID SCIENCE
(2022)
Article
Thermodynamics
Ramsankar Veerakumar, Linchuan Tian, Haiyang Hu, Yang Liu, Hui Hu
Summary: An experimental campaign was conducted to investigate the dynamic icing process and wind loads on an ACSR power cable under dry rime and wet glaze icing conditions. The icing process was recorded using high-resolution imaging, and the 3D shapes of the ice layers were quantified using a novel scanning system. The wind loads on the cable were measured using force/moment transducers and the evolution of the wake flow was analyzed using Particle Image Velocimetry (PIV). Differences were observed in the ice accretion and wind loads between the dry rime and wet glaze icing conditions.
EXPERIMENTAL THERMAL AND FLUID SCIENCE
(2023)
Article
Thermodynamics
Linchuan Tian, Linkai Li, Haiyang Hu, Hui Hu
Summary: An experimental campaign was conducted to study dynamic ice accretion on rotating aeroengine fan blades and evaluate its impact on fan rotor performance. The experiments revealed that ice accretion caused substantial degradation of the fan rotor, particularly under glaze icing conditions. The rougher blade surfaces due to ice accretion negatively affected the performance of the fan rotor. These findings are important for understanding fan performance and designing ice protection systems.
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER
(2023)