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Journal articles on the topic 'Wind tunnel tests'

Author: Grafiati

Published: 4 June 2021

Last updated: 25 July 2025

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1

Bak, Christian, Anders S. Olsen, Andreas Fischer, et al. "Wind tunnel benchmark tests of airfoils." Journal of Physics: Conference Series 2265, no. 2 (2022): 022097. http://dx.doi.org/10.1088/1742-6596/2265/2/022097.

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Abstract This paper describes a benchmark of four airfoils in the Poul la Cour Tunnel (PLCT). The wind tunnel, the corrections used and the method of making adapters for the airfoils are also described. Very good agreement was in general observed between the measurements in PLCT and in other high quality wind tunnels. Some deviations were seen, but they were mainly attributed to the differences in separation on the airfoil. Apart from the benchmarking, this paper also highlights the challenges in testing airfoils in general such as obtaining 2D flow on thick airfoils that inherently shows sepa

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2

Hasan, Mohammed Munif, and Shabudin Mat. "Data Reduction Analysis on UTM-LST External Balance." International Journal for Research in Applied Science and Engineering Technology 10, no. 10 (2022): 952–59. http://dx.doi.org/10.22214/ijraset.2022.47097.

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Abstract: The effective use of wind-tunnel testing in determining aerodynamic properties of a body is very much dependent upon the reliability and speed with which wind-tunnel data can be reduced. The operating efficiency of the wind tunnels is substantially improved by the capability of providing lower aerodynamic coefficients in real time, or online, which decreases the expensive wind-tunnel time necessary for each test. This paper describes a system for presenting reduced wind-tunnel data in real time for UTM-LST. The requirements for data-handling equipment and data reduction procedures fo

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3

Zhang, Ying Chao, Wei Ding, Zhe Zhang, and Jie Li. "Comparison Research on Aerodynamic Drags and Pressure Coefficients of Reference Car Models in Automotive Wind Tunnel." Advanced Materials Research 989-994 (July 2014): 2834–38. http://dx.doi.org/10.4028/www.scientific.net/amr.989-994.2834.

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The aerodynamic drags of different reference car models were investigated to calibrate the performance of the Automotive Wind Tunnel in Jilin University. The two kinds of reference models--MIRA and SAE reference car models were involved in this paper, considering the actual situation of the Automotive Wind Tunnel in Jilin University. The results of the research show that the Automotive Wind Tunnel in Jilin University can meet the demand for automotive wind tunnel tests and it can get the same performances as other wind tunnels have and reliable test data can be obtained in it.

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Zhou, Qi, Yuxiang Zhu, Yu Wang, and Jiceng Han. "CFD-Based Wind Field Correction Method for Terrain Wind Tunnel Tests." Journal of Physics: Conference Series 2083, no. 3 (2021): 032083. http://dx.doi.org/10.1088/1742-6596/2083/3/032083.

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Abstract At present, the wind tunnel test results will have certain deviation and distortion when the wind tunnel test is conducted on certain mountainous terrain with complex local terrain and large variation of wind field characteristics due to the accuracy range of the measuring instruments used in wind tunnel test. In order to correct and obtain correct wind tunnel test results, the wind tunnel tests and numerical simulations were conducted on a super-large bridge in the mountainous area of Southwest China, and the wind parameters of the wind field at the bridge site were obtained. The CFD

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Yang, Aiwei, Dawei Liu, Guangwei Xiang, and Gun Li. "Design of cryogenic balance temperature control system based on MCGS and PLC and analysis of its influence relationship." Journal of Physics: Conference Series 2993, no. 1 (2025): 012024. https://doi.org/10.1088/1742-6596/2993/1/012024.

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Abstract To address the issue of slow temperature adjustment in cryogenic balance, which severely affects the efficiency of wind tunnel tests, this study investigates the temperature control system for cryogenic balance. Considering the wide temperature range and deep cooling requirements of cryogenic wind tunnels, a comprehensive design of the temperature cryogenic was developed. Based on MCGS and PLC, the first domestically developed cryogenic balance temperature control system was implemented. After installation, equipment testing and wind tunnel experiments were conducted. The experimental

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6

Vuković, Đorđe, and Dijana Damljanović. "A technique for reducing supersonic transient loads on internal wind tunnel balances." Tehnika 79, no. 2 (2024): 177–84. http://dx.doi.org/10.5937/tehnika2402177v.

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Design of slender supersonic missiles requires a comprehensive experimental support in the form of wind tunnel data for a wide range of flight parameters (angle of attack and Mach number). However, in supersonic wind tunnel testing, the problem exists of transient loads at the times of the starting and stopping of the supersonic flow. In the environments of pronounced transient loads, characteristic of blowdowin wind tunnels like the T-38 of the Military technical Institute in Belgrade, it is necessary to provide control of the use of internal wind tunnel balances in the permitted design load

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7

MAEDA, Tatsuo, and Yoshihiko KONDO. "RTRI's Large-scale Low-noise Wind Tunnel and Wind Tunnel Tests." Quarterly Report of RTRI 42, no. 2 (2001): 65–70. http://dx.doi.org/10.2219/rtriqr.42.65.

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8

Krzysiak, A. "Bottom drag measurements in experimental wind tunnel tests." Journal of Physics: Conference Series 2367, no. 1 (2022): 012001. http://dx.doi.org/10.1088/1742-6596/2367/1/012001.

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Abstract The paper presents the results of wind tunnel tests aimed at determining the model bottom drag in the case of rocket model tests. The balance measurement technique of the rocket model fixed in the wind tunnel test section by the rear sting was discussed. The model was equipped with the two parallel boosters. Based on the wind tunnel test of the rocket twin model the values of the bottom pressure was determined for tested Mach numbers. An algorithm of wind tunnel corrections was shown, which allowed the total drag determination in a case of the rocket active or passive rocket flight. T

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9

Samali, B., K. C. S. Kwok, G. S. Wood, and J. N. Yang. "Wind Tunnel Tests for Wind-Excited Benchmark Building." Journal of Engineering Mechanics 130, no. 4 (2004): 447–50. http://dx.doi.org/10.1061/(asce)0733-9399(2004)130:4(447).

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10

Jia, Sijia, Zhenkai Zhang, Haibo Zhang, Chen Song, and Chao Yang. "Wind Tunnel Tests of 3D-Printed Variable Camber Morphing Wing." Aerospace 9, no. 11 (2022): 699. http://dx.doi.org/10.3390/aerospace9110699.

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This paper introduces the realization and wind tunnel testing of a novel variable camber wing equipped with compliant morphing trailing edges. Based on the aerodynamic shape and compliant mechanisms that were optimized in advance, a wind tunnel model called mTE4 was developed, in which the rigid leading edge, rigid wing box, and compliant trailing edge were manufactured by 3D printing technology using three different materials. Due to difficulties in the detailed design of a small-scale model, special attention is devoted to the implementation procedure. Additionally, the static and dynamic ch

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11

WANG, Wenjun, Hiroshi KUROYANAGI, and Kazunori YOSHIDA. "1A16 6 Force Component Balance for Wind Tunnel Model Tests." Proceedings of the Symposium on the Motion and Vibration Control 2010 (2010): _1A16–1_—_1A16–7_. http://dx.doi.org/10.1299/jsmemovic.2010._1a16-1_.

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12

MAEDA, Tatsuo. "Wind Tunnel Tests on Railway Vehicles." Wind Engineers, JAWE 34, no. 1 (2009): 24–29. http://dx.doi.org/10.5359/jawe.34.24.

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13

Flamand, Olivier, Philippe Delpech, Pierre Palier, and Jean-Paul Bouchet. "Benefit of Wind Tunnels with Large Test Sections for Wind Engineering Applications." Mathematical Modelling in Civil Engineering 15, no. 2 (2019): 14–19. http://dx.doi.org/10.2478/mmce-2019-0005.

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Abstract Atmospheric Boundary layer wind tunnels (ABLWT) dedicated to building safety and comfort have been operated by CSTB in Nantes since 1971. Because ABLWT only deal with reduced scale models of real structures, the necessity of a larger wind tunnel, the Jules Verne Climatic wind tunnel (CWT), able to reproduce extreme wind loads on real scale structures arose in the years 80. Hence, it became a major European facility operating for improvement of the safety, quality and environmental impact of buildings and civil engineering works as well as products from industrial fields (transportatio

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14

Wang, Lei, Fen Shi, Zheng Wang, and Shuguo Liang. "Blockage Effects in Wind Tunnel Tests for Tall Buildings with Surrounding Buildings." Applied Sciences 12, no. 14 (2022): 7087. http://dx.doi.org/10.3390/app12147087.

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To study the blockage effects in wind tunnel tests for tall buildings with surrounding buildings and establish a reasonable calculation method for the blockage ratio, this paper carried out fifty-one test conditions of pressure model wind tunnel tests with three scale ratios. The tests considered the relative location, relative height, and model number of the surrounding buildings to those of the target building by the rigid pressure models. Based on the wind tunnel tests, the blockage effects on the pressure coefficients and drag coefficients were studied in detail. The results showed that th

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15

Cataldo, José, Valeria Durañona, Rodolfo Pienika, Pablo Pais, and Alfredo Gravina. "Wind damage on citrus fruit study: Wind tunnel tests." Journal of Wind Engineering and Industrial Aerodynamics 116 (May 2013): 1–6. http://dx.doi.org/10.1016/j.jweia.2013.01.008.

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16

Yi, Zijing, Lingjun Wang, Xiao Li, Zhigang Zhang, Xu Zhou, and Bowen Yan. "Computational Fluid Dynamics-Aided Simulation of Twisted Wind Flows in Boundary Layer Wind Tunnel." Applied Sciences 14, no. 3 (2024): 988. http://dx.doi.org/10.3390/app14030988.

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The twisted wind flow (TWF), referring to the phenomenon of wind direction varying with height, is a common feature of atmospheric boundary layer (ABL) winds, noticeably affecting the wind-resistant structural design and the wind environment assessment. The TWF can be effectively simulated by a guide vane system in wind tunnel tests, but the proper design and configuration of the guide vanes pose a major challenge as practical experience in using such devices is still limited in the literature. To address this issue, this study aims to propose an approach to determining the optimal wind tunnel

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17

Dr. G.Venkateswarlu and Tejavath Rajesh. "MODELING AND STATIC AND MODAL ANALYSIS OF FUSELAGE BOMBARDIER CRJ 200 AIRCRAFT USING VARIOUS MATERIALS." International Journal of Engineering, Science and Advanced Technology 24, no. 10 (2024): 419–25. http://dx.doi.org/10.36893/ijesat.2024.v24i10.053.

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This study details the low-speed configuration development process of the CRJ-700, focussing on half-model high Reynolds number wind tunnel tests. The procedure included flight testing, wind tunnel testing, and CFD design and analysis. A 7% scale half-model was used for the experimental development of the flaps and slats in the IAR 5 x 5 ft High Reynolds Number wind tunnel. Decisions taken in the wind tunnel result in a brief and successful flight test program, and the results of these tests correlate extremely well with the data from the flight tests.

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18

Tabatabaei, Narges, Ramis Örlü, Ricardo Vinuesa, and Philipp Schlatter. "Aerodynamic Free-Flight Conditions in Wind Tunnel Modelling through Reduced-Order Wall Inserts." Fluids 6, no. 8 (2021): 265. http://dx.doi.org/10.3390/fluids6080265.

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Parallel sidewalls are the standard bounding walls in wind tunnels when making a wind tunnel model for free-flight condition. The consequence of confinement in wind tunnel tests, known as wall-interference, is one of the main sources of uncertainty in experimental aerodynamics, limiting the realizability of free-flight conditions. Although this has been an issue when designing transonic wind tunnels and/or in cases with large blockage ratios, even subsonic wind tunnels at low-blockage-ratios might require wall corrections if a good representation of free-flight conditions is intended. In order

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19

Popov, Andrei V., Lucian T. Grigorie, Ruxandra Botez, Mahmood Mamou, and Youssef Mebarki. "Real Time Morphing Wing Optimization Validation Using Wind-Tunnel Tests." Journal of Aircraft 47, no. 4 (2010): 1346–55. http://dx.doi.org/10.2514/1.47431.

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20

Selig, Michael S., and Bryan D. McGranahan. "Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines." Journal of Solar Energy Engineering 126, no. 4 (2004): 986–1001. http://dx.doi.org/10.1115/1.1793208.

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This paper presents detailed wind tunnel tests data taken on six airfoils having application to small wind turbines. In particular, lift, drag and moment measurements were taken at Reynolds numbers of 100,000, 200,000, 350,000 and 500,000 for both clean and rough conditions. In some cases, data were also taken at a Reynolds number of 150,000. The airfoils included the E387, FX 63-137, S822, S834, SD2030, and SH3055. Prior to carrying out the tests, wind tunnel flow quality measurements were taken to document the low Reynolds number test environment. Oil flow visualization data and performance

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21

Bosak, Grzegorz. "Wind tunnel tests of wind action on a high-rise building." Budownictwo i Architektura 13, no. 2 (2014): 163–71. http://dx.doi.org/10.35784/bud-arch.1891.

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The paper summarizes the results of wind tunnel tests of a wind action on a high-rise building design in Warsaw. Measurements were accomplished in Wind Engineering Laboratory of Cracow University of Technology. Wind pressures on external surfaces of the building model were acquired. A study of the character of the wind action on a tower of the building was the main aim of the paper. A triangle shape with rounded corners of the cross section of the tower and a complex group of neighbor buildings support aerodynamic analysis in a wind tunnel. Wind pressure coefficients on the external building s

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22

Vyalkov, Andrey Viktorovitch. "INERTIAL TECHNOLOGY OF WIND TUNNEL SPIN TESTS." TsAGI Science Journal 47, no. 5 (2016): 537–52. http://dx.doi.org/10.1615/tsagiscij.2017019332.

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23

Warnitchai, Pennung, Suksit Sinthuwong, and Kobchai Poemsantitham. "Wind Tunnel Model Tests of Large Billboards." Advances in Structural Engineering 12, no. 1 (2009): 103–14. http://dx.doi.org/10.1260/136943309787522650.

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24

Belloli, Marco, Federico Cheli, Ilmas Bayati, Stefano Giappino, and Fabio Robustelli. "Handbike Aerodynamics: Wind Tunnel Versus Track Tests." Procedia Engineering 72 (2014): 750–55. http://dx.doi.org/10.1016/j.proeng.2014.06.127.

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25

Zhao, Xiaoyi, Zhile Shu, and Xiangjun Pei. "Research and Perspectives on Fire-Fighting Systems in Tunnels under Strong Piston Wind Action." Buildings 13, no. 2 (2023): 435. http://dx.doi.org/10.3390/buildings13020435.

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Guided by the technical requirements for tunnel fire safety, an overview of tunnel piston wind, combustion models, and full-size and small tunnel fire tests is presented. Firstly, the theoretical model and numerical calculation methods for piston wind tunnel fires are presented from the perspective of numerical simulation. Then, full-scale and small-scale test models for tunnel fires are presented, and the advantages and disadvantages of single-row, multi-row, single-fire source, and multi-fire source test methods are described. Finally, key breakthrough directions for future numerical and exp

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26

MIZUNO, Takeshi, Yasuhiro SAKAI, Masaya TAKASAKI, and Yuji ISHINO. "A103 Wind-Tunnel for Spinning Body Using Magnetic Suspension : 5th report: Wind-tunnel Tests." Proceedings of the Symposium on the Motion and Vibration Control 2011.12 (2011): 29–32. http://dx.doi.org/10.1299/jsmemovic.2011.12.29.

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27

Migliore, Paul, and Stefan Oerlemans. "Wind Tunnel Aeroacoustic Tests of Six Airfoils for Use on Small Wind Turbines*." Journal of Solar Energy Engineering 126, no. 4 (2004): 974–85. http://dx.doi.org/10.1115/1.1790535.

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Aeroacoustic tests of seven airfoils were performed in an open jet anechoic wind tunnel. Six of the airfoils are candidates for use on small wind turbines operating at low Reynolds numbers. One airfoil was tested for comparison to benchmark data. Tests were conducted with and without boundary layer tripping. In some cases, a turbulence grid was placed upstream in the test section to investigate inflow turbulence noise. An array of 48 microphones was used to locate noise sources and separate airfoil noise from extraneous tunnel noise. Trailing-edge noise was dominant for all airfoils in clean t

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Yu, Li, Bin Bin Lv, Yu Yan, Hong Tao Guo, Jun Zha, and Chang Rong Zhang. "Introduction to Automatic Shutdown System for Flutter Test of High Speed Wind Tunnel." Advanced Materials Research 1030-1032 (September 2014): 1584–87. http://dx.doi.org/10.4028/www.scientific.net/amr.1030-1032.1584.

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This paper introduces an automatic shutdown system for model protection during the flutter test in high speed wind tunnels. This automatic shutdown system can be used to determine any unsafe condition through model flutter signals before triggering shutdown of wind tunnels, solving problems of delayed response and mistakes happen during manual measurement of subcritical state of model flutter. The reliability and effectiveness of this system have been proved good via wind tunnel tests, hence the possibility of damage to the model caused by flutter during the flutter test of high speed wind tun

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Yang, Wei, Meng Yu, Bowen Yan, et al. "Wind Tunnel Tests of Wake Characteristics for a Scaled Wind Turbine Model Based on Dynamic Similarity." Energies 15, no. 17 (2022): 6165. http://dx.doi.org/10.3390/en15176165.

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This wind tunnel study was conducted to investigate the similarity laws involved in the reasonable simulation of the wake characteristics of a full-scale wind turbine. A 5 MW scaled wind turbine model was designed using an optimization method based on the blade element momentum (BEM) theory. Subsequently, wind tunnel tests were carried out on the geometrically similar model and the thrust-optimized model, with different yaw angles and under various upstream flow conditions. The results indicated that the wake development of the wind turbine model was closely related to the thrust forces of the

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30

Li, Chunguang, Yan Han, Ji Zhang, Shuqian Liu, and C. S. Cai. "Wind Tunnel Tests on Wind Pressure Characteristics of Sawtooth Roofs." Journal of Aerospace Engineering 31, no. 6 (2018): 04018107. http://dx.doi.org/10.1061/(asce)as.1943-5525.0000931.

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31

Verelst, D. R. S., T. J. Larsen, and J. W. van Wingerden. "Wind tunnel tests of a free yawing downwind wind turbine." Journal of Physics: Conference Series 555 (December 16, 2014): 012103. http://dx.doi.org/10.1088/1742-6596/555/1/012103.

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32

Liu, Xianzhi, Yan Han, C. S. Cai, Marc Levitan, and Dimitris Nikitopoulos. "Wind tunnel tests for mean wind loads on road vehicles." Journal of Wind Engineering and Industrial Aerodynamics 150 (March 2016): 15–21. http://dx.doi.org/10.1016/j.jweia.2015.12.004.

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Tsutsumi, J., T. Katayama, and M. Nishida. "Wind tunnel tests of wind pressure on regularly aligned buildings." Journal of Wind Engineering and Industrial Aerodynamics 43, no. 1-3 (1992): 1799–810. http://dx.doi.org/10.1016/0167-6105(92)90592-x.

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34

Tse, K. T., A. U. Weerasuriya, and K. C. S. Kwok. "Simulation of twisted wind flows in a boundary layer wind tunnel for pedestrian-level wind tunnel tests." Journal of Wind Engineering and Industrial Aerodynamics 159 (December 2016): 99–109. http://dx.doi.org/10.1016/j.jweia.2016.10.010.

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35

Damljanović, Dijana, Đorđe Vuković, Goran Ocokoljić, and Boško Rašuo. "New Transonic Tests of HB-2 Hypersonic Standard Models in the VTI T-38 Trisonic Wind Tunnel." Aerospace 12, no. 2 (2025): 131. https://doi.org/10.3390/aerospace12020131.

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Recent experience has shown that test results of standard wind tunnel models under off-design conditions could be a useful aid in preparations of some nonstandard wind tunnel tests. However, reference data for such conditions do not exist, or they are scarce. Therefore, off-design transonic wind tunnel tests of the HB-2 standard models were executed in the VTI T-38 wind tunnel as a supplement to the supersonic tests of the same models under design-intent conditions, for which reference results were available. New tests were conducted so that test envelopes partially overlapped with those from

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36

Zhao, Yi, Ruibin Li, Lu Feng, Yan Wu, and Naiping Gao. "Boundary layer wind tunnel tests of outdoor airflow field around urban buildings: A review of methods and status." E3S Web of Conferences 356 (2022): 04031. http://dx.doi.org/10.1051/e3sconf/202235604031.

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Outdoor airflow fields have received increasing attention in the building aerodynamics community due to that the airflow distributions around outdoor buildings are closely related to issues such as thermal comfort, building ventilation, and pollutant dispersion. The focus of this paper is on the airflow distributions around buildings obtained through wind tunnel tests, and such studies are mostly conducted in boundary layer wind tunnel with long test section. This paper reviews current techniques for boundary layer wind tunnel tests of airflow distributions in urban outdoor environments. Then,

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Du, Yufeng, Lulu Wang, Jilong Zhu, Weizhong Wang, Neng Xiong, and Danping Guo. "Uncertainty analysis method of high-speed wind tunnel standard model test results based on GUM and MCM." Journal of Physics: Conference Series 2851, no. 1 (2024): 012020. http://dx.doi.org/10.1088/1742-6596/2851/1/012020.

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Abstract The standard model is a standard calibration model that has a well-known geometric shape and can represent the aerodynamic layout characteristics of a certain type of aircraft. It has many functions, including evaluating the accuracy of wind tunnel test data, verifying the integrity of the wind tunnel flow field and measurement system, and developing and verifying wind tunnel test technology. Conducting wind tunnel tests using standard models is a key step in realizing the functions of standard models. However, all existing literature on standard model tests has not effectively evalua

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Muggiasca, Sara, Federico Taruffi, Alessandro Fontanella, Simone Di Carlo, and Marco Belloli. "Aerodynamic and Structural Strategies for the Rotor Design of a Wind Turbine Scaled Model." Energies 14, no. 8 (2021): 2119. http://dx.doi.org/10.3390/en14082119.

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Experimental tests performed in a wind tunnel or in a natural laboratory represent a fundamental research tool to develop floating wind technologies. In order to obtain reliable results, the wind turbine scale model rotor must be designed so to obtain a fluid-structure interaction comparable to the one experienced by a real machine. This implies an aerodynamic design of the 3D blade geometry but, also, a structural project to match the main aeroelastic issues. For natural laboratory models, due to not controlled test conditions, the wind turbine rotor model must be checked also for extreme win

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Belostotsky, Alexander, Pavel Akimov, and Irina Afanasyeva. "ABOUT “LEGITIMIZATION” OF NUMERICAL MODELLING OF WIND IMPACTS ON BUILDINGS AND STRUCTURES IN DESIGN CODES." International Journal for Computational Civil and Structural Engineering 15, no. 4 (2019): 14–24. http://dx.doi.org/10.22337/2587-9618-2019-15-4-14-24.

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The distinctive paper is detoded to problem of “legitimization” of numerical modelling of wind loads and impacts on buildings and structures. General information about computational fluid dynamics (CFD) and its development prospects is presented. The main advantages and disadvantages of numerical simulation compared with tests in wind tunnels (wind tunnel tests) are considered. Besides, information about the second modification of corresponding Russian design codes (SP 20.13330.2016 “SNiP 2.01.07-85* Loads and effects”) is provided. Prospects for the further development of numerical modelling

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Yuejun, Liu, Tang Ai P., Liu Ke T., and Tu Jie W. "The Aerodynamic Analysis for Iced Four Bundled Transmission Lines with Typical Crescent." Open Electrical & Electronic Engineering Journal 8, no. 1 (2014): 84–89. http://dx.doi.org/10.2174/1874129001408010084.

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Despite the fact that the wind tunnel tests have been carried out on iced transmission lines subjected to wind load, it is not practical to do wind tunnel tests due to its high cost. This paper describes a detailed numerical simulation method that can be used to instead of wind tunnel tests. Based on the galloping mechanism of iced transmission lines, the aerodynamic test was simulated with the typical crescent super-large thickness iced four bundled conductors. One of the results highlighted in this study is that the wind angle of attack had significant influence on the aerodynamics of iced c

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Ma, Ziqing, Ewoud J. J. Smeur, and Guido C. H. E. de Croon. "Wind tunnel tests of a wing at all angles of attack." International Journal of Micro Air Vehicles 14 (January 2022): 175682932211109. http://dx.doi.org/10.1177/17568293221110931.

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Tailsitters have complex aerodynamics that make them hard to control throughout the entire flight envelope, especially at very high angle of attack (AoA) and reverse flow conditions. The development of controllers for these vehicles is hampered by the absence of publicly available data on forces and moments experienced in such conditions. In this paper, wind tunnel experiments are performed under different flap deflections and throttle settings at all possible AoA. The dataset is made open access. Our analysis of the data shows for the tested wing, flap deflections greatly affect the lift coef

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Krzysiak, Andrzej. "Wind Tunnel Tests of Damage to the Tu-154M Aircraft Wing." Journal of Aerospace Engineering 32, no. 6 (2019): 04019083. http://dx.doi.org/10.1061/(asce)as.1943-5525.0001087.

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He, YC, JCK Cheung, QS Li, and JY Fu. "Accurate determination of reference wind speed and reference static pressure in wind tunnel tests." Advances in Structural Engineering 23, no. 3 (2019): 578–83. http://dx.doi.org/10.1177/1369433219875302.

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The reference wind speed and reference static pressure are two key parameters for determining the testing results of wind tunnel experiments. Traditionally, the values of these parameters can be determined using direct measurement methods. However, such methods may suffer from less accuracy and inconvenience of operations. This article documents an indirect measurement method which, compared to the traditional methods, has the merits of higher accuracy and greater operational convenience. Examples are presented to demonstrate the main procedures of the method and typical findings by using the

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Yao, Jianfeng, Guohui Shen, Zhibin Tu, Yong Chen, and Wenjuan Lou. "Wind Tunnel Tests of an Aeroelastic Model of a Long-Span Transmission Tower." Sustainability 14, no. 18 (2022): 11613. http://dx.doi.org/10.3390/su141811613.

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The modal analysis of a long-span transmission tower was carried out using a finite element method, and then its aeroelastic model was established by the discrete stiffness method for wind tunnel tests. The displacement and acceleration of the aeroelastic model were measured by a vision-based displacement measuring instrument and accelerometer, respectively. Also, the wind-induced responses of the tower were conducted by finite element calculation, with which the results of the wind tunnel tests are compared. The gust response factor was calculated and compared with those from the specificatio

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Shen, Lihua, Xu Cui, Biling Wang, Qiang Li, and Jin Guo. "Improved African Vulture Optimization Algorithm for Optimizing Nonlinear Regression in Wind-Tunnel-Test Temperature Prediction." Processes 13, no. 7 (2025): 1956. https://doi.org/10.3390/pr13071956.

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The thermal data of the hypersonic wind tunnel field accurately reflect the aerodynamic performance and key parameters of the aircraft model. However, the prediction of the temperature in hypersonic wind tunnels has problems such as a large delay, nonlinearity and multivariable coupling. In order to reduce the influence brought by temperature changes and improve the accuracy of temperature prediction in the field control of hypersonic wind tunnels, this paper first combines kernel principal component analysis (KPCA) with phase space reconstruction to preprocess the temperature data set of wind

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Galinski, Cezary, Grzegorz Krysztofiak, Marek Miller, et al. "Wind tunnel tests of the inverted joined wing and a comparison with CFD results." Aircraft Engineering and Aerospace Technology 90, no. 4 (2018): 586–601. http://dx.doi.org/10.1108/aeat-11-2016-0195.

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Purpose The purpose of this paper is to present the methodology and approach adapted to conduct a wind tunnel experiment on the inverted joined-wing airplane flying model together with the results obtained. Design/methodology/approach General assumptions underlying the dual-use model design are presented in this paper. The model was supposed to be used for both wind tunnel tests and flight tests that significantly drive its size and internal structure. Wind tunnel tests results compared with the outcome of computational fluid dynamics (CFD) were used to assess airplane flying qualities before

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KATAGIRI, Junji. "Wind Tunnel Tests for Wind Resistance Design of High-rise Buildings." Wind Engineers, JAWE 34, no. 1 (2009): 10–17. http://dx.doi.org/10.5359/jawe.34.10.

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Llorente, E., A. Gorostidi, M. Jacobs, W. A. Timmer, X. Munduate, and O. Pires. "Wind Tunnel Tests of Wind Turbine Airfoils at High Reynolds Numbers." Journal of Physics: Conference Series 524 (June 16, 2014): 012012. http://dx.doi.org/10.1088/1742-6596/524/1/012012.

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Jing, Xiao-kun, and Yuan-qi Li. "Wind Tunnel Tests for Wind Pressure Distribution on Gable Roof Buildings." Scientific World Journal 2013 (2013): 1–11. http://dx.doi.org/10.1155/2013/396936.

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Gable roof buildings are widely used in industrial buildings. Based on wind tunnel tests with rigid models, wind pressure distributions on gable roof buildings with different aspect ratios were measured simultaneously. Some characteristics of the measured wind pressure field on the surfaces of the models were analyzed, including mean wind pressure, fluctuating wind pressure, peak negative wind pressure, and characteristics of proper orthogonal decomposition results of the measured wind pressure field. The results show that extremely high local suctions often occur in the leading edges of longi

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Kong, L., and G. V. Parkinson. "A 3-D tolerant wind tunnel for general wind engineering tests." Journal of Wind Engineering and Industrial Aerodynamics 69-71 (July 1997): 975–85. http://dx.doi.org/10.1016/s0167-6105(97)00221-3.

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