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CONTENTS
Volume 40, Number 3, March 2025
 


Abstract
Since the 1970s, winglet devices have been widely utilized to ameliorate the aerodynamic performance of aircraft by increasing L/D of the wing configuration. Modern designs can change cant angle during the flight in order to maximize their benefits to all flight states, which is limited to on-design points in passive/fixed designs. This paper discusses the effects of atmospheric and operating parameters on the aeroacoustics of a double-swept wing configuration facilitated with a rotary winglet device. To do so, the turbulent flow is simulated via 3D RANS formulation and k-ω SST turbulence model. Then, machine learning tools, consisting of Multi-layer Perceptron (MLP) neural networks and supervised classification methods are used to generate scaler regression models based upon numerical aeroacoustic datasets. Moreover, deep Convolutional Neural Network (CNN) is used to estimate the aeroacoustic field. The results depicted that changing the cant angle significantly affects the aerodynamic noise of the wing configuration regardless of operating conditions. Secondly, artificial intelligence is a practical modeling tool for acoustic parameters with reasonable accuracy and cost compared with RANS simulations.

Key Words
aircraft noise; CFD simulation; machine learning; Regression Analysis; rotary winglets; supervised classification

Address
Erfan Vaezi:Department of Aerospace Engineering, Sharif University of Technology, Azadi Avenue, Tehran 14588-89694, Tehran, Iran

S. Amirreza S. Madani:Department of Aerospace Engineering, Delft University of Technology, Kluyverweg 1, 2629 HS Delft, The Netherlands

Abstract
The NIST-UWO database has pressure coefficient time-history data, encompassing various roof slopes, eave heights, terrain exposures, and wind angles. Utilizing SAP2000 to obtain the influence coefficients (IC) for eave and ridge moments and displacements, corresponding critical moment and displacement coefficients were computed for three different gable roof pitch (1/4:12,1:12, and 3:12) models each having three different eave heights of 7.32 m, 9.75 m, and 12.19 m, in two terrain types – open country and suburban. The study utilized Decision Tree (DT), Random Forest (RF), and Extreme Gradient Boosting (XGBoost) to predict these load effect coefficients for potential missing wind angles. Additionally, the study compared these machine learning models' performance in handling exposure categories as numerical values (roughness length) and categorical variables (represented via one-hot encoding). The results showed that all models performed consistently well, regardless of exposure category representation, with XGBoost demonstrating better performance compared to RF and DT.

Key Words
machine learning; NIST-UWO aerodynamic database; wind load effects

Address
Manoj Adhikari:Department of Civil and Environmental Engineering, Rensselaer Polytechnic Institute, Troy, NY, U.S.A.

Christopher W. Letchford:Department of Civil and Environmental Engineering, Rensselaer Polytechnic Institute, Troy, NY, U.S.A.

Abstract
Super-large cooling tower is a kind of typical high-rise, large-span and wind-sensitive structure. The interaction between the lower foundation structure of the tower and soil mass influences wind-induced vibration performances of the tower body significantly. Nevertheless, the structure-pile foundation-soil coupling effect of the cooling tower is ignored in existing norms. The value of wind-induced vibration coefficient cannot accurately reflect the wind-induced vibration performances of the structure under wind load. Three different models of structure-pile foundation-soil finite element coupling effects were built for a systematic quantitative study of influences of tower structure-soil coupling modeling techniques on the dynamic characteristics and wind-induced vibration responses of the cooling tower. These three models are direct solidification between the herringbone columns and soil mass (Model I), coupling effect of herringbone columns, circumferential base (beam element) and pile foundation (soil spring) (Model II), and coupling effect of herringbone columns, circumferential base (solid element), pile foundation (base element) and soil mass (Model III). A comparative analysis on displacement of tower body and responses to internal force under wind loads was carried out. The value standard of wind-induced vibration coefficient under different target responses was discussed. Results demonstrate that the structural fundamental frequency of Model I is 0.884Hz, while the fundamental frequencies of Model II and Model III are decreased by 7.89% and 18.8%. For the maximum displacement of cooling tower under dead load and static wind load, Model I <Model II<Model III.The maximum error of response extremum of three cooling tower models to the meridian axial force under pulsation wind load is only 2.65%. The maximum means of radial displacement and circumferential bending moment are Model I<Model II< Model III.The Model I shows the lowest wind induced vibration coefficient under the response goals of radial displacement and circumferential bending moment, followed by Model II and Model III successively. On this basis, a value standard of two-dimensional interval wind-induced vibration coefficient for super-large cooling tower considering structure-pile foundation-soil coupling effect was established, which could provide scientific reference for wind-resistant design of similar structures.

Key Words
super-large cooling tower; structure-pile foundation-soil coupling effect; wind load; wind-induced vibration response; wind-induced vibration coefficient

Address
Sainan Zeng:Department of Civil and Airport Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

Shitang Ke:Department of Civil and Airport Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

Yifan Qi:Department of Civil and Airport Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

Yan Qin:Department of Civil and Airport Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China

Xiaoqing Gu:China Energy Engineering Group Jiangsu Power Design Institute Co., LTD, Nanjing 211102, China

Jiaqing Shu:China Energy Engineering Group Jiangsu Power Design Institute Co., LTD, Nanjing 211102, China

Abstract
Surface roughness reflects the obstructive effect of surface features on atmospheric turbulence, and is a key factor influencing the characterization of the near-surface wind field. In this study, the method for measuring roughness in the atmospheric boundary layer was introduced to investigate the effect of surface roughness on the wind profile shape and turbulence characteristics of downbursts. Different roughness landforms in nature were simulated by arranging roughness elements with various sizes and distribution densities. Subsequently, wind field experiments of the downburst outflow section were carried out. The results show that roughness has a strong decay effect on streamwise wind speed; as the surface roughness increases, the vertical height corresponding to the maximum wind speed increases. Meanwhile, the turbulence intensity in the inner layer of the wall jet increases significantly, but the turbulence intensity in the outer layer decreases gradually. To address the problem that the existing empirical models of vertical wind profiles for horizontal wind speeds of downburst are unsuitable for all rough landforms, equations for fitting vertical wind profiles for different rough landforms are proposed. In addition, the surface roughness significantly affects the Reynolds stress in the inner layer of the wall jet. The analysis reveals that the wall jet still follows a dimensionless law in high Reynolds number tests with different surface roughness. The study further provides some references for downburst wind loads considering roughness.

Key Words
surface roughness; wall jet; wind field characteristic; wind profile; wind tunnel test

Address
Yongli Zhong:School of Civil and Hydraulic Engineering, Chongqing University of Science and Technology, Chongqing 401331, China

Yichen Liu:School of Civil and Hydraulic Engineering, Chongqing University of Science and Technology, Chongqing 401331, China

Bowei Liu:School of Civil and Hydraulic Engineering, Chongqing University of Science and Technology, Chongqing 401331, China

Xiangjun Tan:School of Civil and Hydraulic Engineering, Chongqing University of Science and Technology, Chongqing 401331, China

Zhitao Yan:1)School of Civil and Hydraulic Engineering, Chongqing University of Science and Technology, Chongqing 401331, China 2)School of Civil Engineering, Chongqing University, Chongqing 400045, China

Xiaogang Yang:School of Civil and Hydraulic Engineering, Chongqing University of Science and Technology, Chongqing 401331, China

Abstract
Wind loads on tall buildings equipped with innovative Porous Double-Skin Facade (PDSF) systems of various porosities were experimentally studied on a small-scale building model. The focus was on integral aerodynamic loads of a tall building equipped with PDSF systems of the 25%, 50% and 65% porosity. This structural design is highly relevant for engineering practice as it encompasses the range of the PDSF porosities that may occur in practice. The building model characterized by a smooth surface was assessed as a reference case. The analysis was performed for suburban wind conditions as a representative of atmospheric conditions characteristic of tall buildings. Wind conditions were studied at the 0° <<a < 45° flow incidence angles. Aerodynamic loads on the building model were analyzed using a high-frequency force balance. Pressure distribution on the inner (non-porous) facade was studied based on pressure measurements. The results obtained in these unique configurations reveal some important findings relevant both for design practice and scholarly research. The most notable results indicate that the maximum mean across-wind moment and its respective maximum standard deviation are lower for all studied PDSF systems compared to the smooth building model. The effect of the PDSF systems on the mean along-wind moment and the respective standard deviation of the building models is negligible. This indicates that the PDSF systems on tall buildings of the studied (bluff body) type do not yield any adverse aerodynamic effects regarding both major aerodynamic moments. On the contrary, the aerodynamic effects observed are favorable, thus a clear benefit for engineering design of tall buildings. In addition to the exhibited integral aerodynamic effects, there are also some important local features to be noted. There is the effect of the PDSF porosity on surface pressure distribution on the inner building model surface, where the less porous outer facade yields a decrease in the mean pressure on the windward inner facade, as much as 20%. In general, there are no adverse effects of the PDSF systems on the overall wind loads on tall buildings, while they may even benefit from the PDSF systems regarding their aerodynamic characteristics.

Key Words
aerodynamic characteristics; porous double-skin facade; tall buildings; wind-tunnel experiments

Address
Petar Skvorc:Faculty of Mechanical Engineering and Naval Architecture, University of Zagreb, Ivana Lucica 5, 10000 Zagreb, Croatia

Andrea Giachetti:Department of Civil and Environmental Engineering, University of Florence, Via di Santa Marta 3, 50139 Florence, Italy

Gianni Bartoli:Department of Civil and Environmental Engineering, University of Florence, Via di Santa Marta 3, 50139 Florence, Italy

Hrvoje Kozmar:Faculty of Mechanical Engineering and Naval Architecture, University of Zagreb, Ivana Lucica 5, 10000 Zagreb, Croatia


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