Gotowe bibliografie tematyczne / Wind tunnel

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Gotowa bibliografia na temat „Wind tunnel”

Autor: Grafiati

Data publikacji: 4 czerwca 2021

Data aktualizacji: 25 lipca 2025

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Artykuły w czasopismach na temat "Wind tunnel"

Andreas, Edgar L., and Larry Mahrt. "On the Prospects for Observing Spray-Mediated Air–Sea Transfer in Wind–Water Tunnels." Journal of the Atmospheric Sciences 73, no. 1 (2015): 185–98. http://dx.doi.org/10.1175/jas-d-15-0083.1.

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Abstract Nature is wild, unconstrained, and often dangerous. In particular, studying air–sea interaction in winds typical of tropical cyclones can place researchers, their instruments, and even their research platforms in jeopardy. As an alternative, laboratory wind–water tunnels can probe 10-m equivalent winds of hurricane strength under conditions that are well constrained and place no personnel or equipment at risk. Wind–water tunnels, however, cannot simulate all aspects of air–sea interaction in high winds. The authors use here the comprehensive data from the Air–Sea Interaction Salt Wate

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Liu, Jie, Yimeng Wu, Zhanyou Sa, et al. "Study on the influence of cross-section shape on the characteristics of wind flow field in heavy-daty railway tunnel." E3S Web of Conferences 536 (2024): 01024. http://dx.doi.org/10.1051/e3sconf/202453601024.

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In order to reduce the coal dust pollution when the heavy train enters the tunnel and to ensure the safety of railroad operation, this paper adopts numerical simulation to study the characteristics of the wind flow field of the heavy train passing through different shapes of tunnels. The results show that the shape of the tunnel section has a significant effect on the piston wind characteristics of the train entering the tunnel. When the train passes through the tunnel, the value of the wind pressure and the gradient of the pressure on the surface of the carriages increase from horseshoe shape

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Yao, Yahu. "Numerical Simulation Analysis of the Influence of Entrance Wind Speed on the Wind Speed Distribution of Coal Mine Tunnel Sections." Academic Journal of Science and Technology 7, no. 3 (2023): 208–12. http://dx.doi.org/10.54097/ajst.v7i3.13399.

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In order to further accurately obtain the wind speed of coal mine tunnels and achieve intelligent ventilation, taking the Wuhushan coal mine tunnel as the research object, the COMSOL Multiphysics numerical simulation software was used to simulate and analyze the influence of inlet wind speed on the wind speed distribution on the tunnel section, and the wind speed distribution law of the semi circular arch tunnel section under different inlet wind speed conditions was obtained. The research results indicate that the wind speed contour is basically parallel to the tunnel wall, and the wind speed

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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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Ma, Xiaojun, Yu Zhao, Xueying Wen, and Jiujiu Chen. "Accessibility Study of a Compact Wind Tunnel with an Unequal Spacing Grid for the Outdoor Wind Environment." Buildings 12, no. 12 (2022): 2188. http://dx.doi.org/10.3390/buildings12122188.

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One of the key issues in architectural design and regional planning is to create a safe and comfortable outdoor building environment, which calls for more studies. Wind tunnel experiments and computational fluid dynamic (CFD) simulations are the primary methods for the current studies. The airflow and boundary conditions are controllable for the wind tunnel experiment, and the data is reliable. In most wind tunnel platforms, spires and roughness elements are applied to create the gradient wind of the atmospheric boundary layer, leading to the oversized, high construction cost, and complex oper

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Allan, M. R., K. J. Badcock, G. N. Barakos, and B. E. Richards. "Wind-tunnel interference effects on a 70° delta wing." Aeronautical Journal 108, no. 1088 (2004): 505–13. http://dx.doi.org/10.1017/s0001924000000336.

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Abstract This paper considers the effects of both wind-tunnel walls and a downstream support structure, on the aerodynamics of a 70° delta wing. A RANS model of the flow was used with the wind-tunnel walls and supports being modelled with inviscid wall boundary conditions. A consistent discretisation of the domain was employed such that grid dependence effects were consistent in all solutions, thus any differences occurring were due to varying boundary conditions (wall and support locations). Comparing solutions from wind-tunnel simulations and simulations with farfield conditions, it has been

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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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Flaga, Andrzej, and Łukasz Flaga. "Research capabilities of the four wind tunnels of the Wind Engineering Laboratory of Cracow University of Technology." Inżynieria i Budownictwo LXXXI, no. 2 (2025): 99–105. https://doi.org/10.5604/01.3001.0055.0912.

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Wind Engineering Laboratory of the Cracow University of Technology (WEL CUT) is a unique and appreciated internationally research and teaching unit in Poland. WEL CUT specializes in research in building aerodynamics, snow engineering, wind power and environmental engineering. The new structure of WEL CUT consists of four wind tunnels: tunnel TA1 – simulation of boundary layer, research on building aerodynamics, wind energy, sport; tunnel TA2 – simulation of climatic conditions, including rainfall, drizzle, artificial snow, and icing; tunnel TA3 – calibration of measuring equipment and wind flo

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Wang, Fei, Xingsen He, Lin Xu, Shengzhong Zhao, and Miaocheng Weng. "Train-Induced Unsteady Airflow in a Metro Tunnel with a Ventilation Shaft." Applied Sciences 14, no. 20 (2024): 9177. http://dx.doi.org/10.3390/app14209177.

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To ensure only one train operates in each ventilation section within an extra-long tunnel, a ventilation shaft was typically installed to divide the entire tunnel into multiple sections. Given the crucial role of piston wind in the metro tunnel environment and ventilation, a deeper understanding of train-induced unsteady airflow in a metro tunnel with a ventilation shaft is desirable. This study uses the unsteady flow theory of the Bernoulli equation to mathematically model piston wind in metro tunnels both with and without ventilation shafts. The influence of various shaft parameters on pisto

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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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Rozprawy doktorskie na temat "Wind tunnel"

Premnath, S. M. Jason. "A tolerant axisymmetric wind tunnel." Thesis, University of British Columbia, 1988. http://hdl.handle.net/2429/28511.

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A solution to the current problem of wind tunnel wall interference could be achieved by ventilating the test section and thereby controlling the flow pattern around the model. The motivation for the slotted wall test section arises from the fact that a fully open jet and a fully closed jet introduce corrections of opposite sign to the wind tunnel data. This current work is limited to axisymmetric wind tunnels and solid blockage corrections. Such a tolerant axisymmetric wind tunnel (TAWT), which does not need any correction to the measured flow quantities and which is also independent of the t

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Mujica, Fernández Fernando R. (Fernando René). "Lattice gas wind tunnel." Thesis, Massachusetts Institute of Technology, 1991. http://hdl.handle.net/1721.1/13444.

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Hickle, Curtis. "Wind Tunnel renovation, flow verification and flapping wing analysis." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://library.nps.navy.mil/uhtbin/hyperion/06Jun%5FHickle.pdf.

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Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, June 2006.<br>Thesis Advisor(s):Dr. Kevin Jones and Dr. Garth Hobson. "June 2006." Includes bibliographical references (p.79-81). Also available in print.

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Paul, Matthew G. "Wing Deflection Analysis of 3D Printed Wind Tunnel Models." DigitalCommons@CalPoly, 2017. https://digitalcommons.calpoly.edu/theses/1751.

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This work investigates the feasibility of producing small scale, low aerodynamic loading wind tunnel models, using FDM 3D printing methods, that are both structurally and aerodynamically representative in the wind tunnel. To verify the applicability of this approach, a 2.07% scale model of the NASA CRM was produced, whose wings were manufacturing using a Finite Deposition Modeling 3D printer. Experimental data was compared to numerical simulations to determine percent difference in wake distribution and wingtip deflection for multiple configurations. Numerical simulation data taken in the form

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Danis, Reed. "Investigating Forward Flight Multirotor Wind Tunnel Testing in a 3-by 4-foot Wind Tunnel." DigitalCommons@CalPoly, 2018. https://digitalcommons.calpoly.edu/theses/1909.

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Investigation of complex multirotor aerodynamic phenomena via wind tunnel experimentation is becoming extremely important with the rapid progress in advanced distributed propulsion VTOL concepts. Much of this experimentation is being performed in large, highly advanced tunnels. However, the proliferation of this class of vehicles extends to small aircraft used by small businesses, universities, and hobbyists without ready access to this level of test facility. Therefore, there is a need to investigate whether multirotor vehicles can be adequately tested in smaller wind tunnel facilities. A tes

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Engel, Mark A. "A wind tunnel investigation of a wing-tip trailing vortex." Thesis, This resource online, 1995. http://scholar.lib.vt.edu/theses/available/etd-01102009-063459/.

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Fitzgerald, Ryan Elizabeth. "Wind tunnel blockage corrections for propellers." College Park, Md.: University of Maryland, 2007. http://hdl.handle.net/1903/7363.

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Thesis (M.S.) -- University of Maryland, College Park, 2007.<br>Thesis research directed by: Dept. of Aerospace Engineering. Title from t.p. of PDF. Includes bibliographical references. Published by UMI Dissertation Services, Ann Arbor, Mich. Also available in paper.

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Lubitz, William David. "Near real time wind energy forecasting incorporating wind tunnel modeling /." For electronic version search Digital dissertations database. Restricted to UC campuses. Access is free to UC campus dissertations, 2005. http://uclibs.org/PID/11984.

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Conan, Boris. "Wind resource accessment in complex terrain by wind tunnel modelling." Phd thesis, Université d'Orléans, 2012. http://tel.archives-ouvertes.fr/tel-00843645.

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To benefit from strong winds, an increasing number of wind turbines are placed in complex terrains. But complex terrains means complex flows and difficult wind resource assessment. This study proposed to use wind tunnel modelling to evaluate the wind in a complex topography. The goal of this study is to evaluate the possibilities of wind resources assessment by wind tunnel modelling and to quantify the important modelling parameters. The lower part of the atmosphere, the atmospheric boundary layer (ABL) is defined by a velocity and a turbulence gradient. The ABL is reproduced in the wind tunne

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Oliveira, Henrique Balona de Sá. "Wind erosion of biochar-amended soil: a wind tunnel experiment." Master's thesis, Universidade de Aveiro, 2014. http://hdl.handle.net/10773/14312.

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Mestrado em Engenharia do Ambiente<br>Biochar application to soils has been reported in the scientific community as a possible means of improving agricultural productivity and, at the same time, as a powerful tool for carbon sequestration and climate change mitigation. However, current knowledge of biochar effects on soil functions and possible environmental threats is still not enough for a full-scale implementation. Erosion is one of the most serious and irreversible threats to soil and there is still no information if biochar may increase or decrease soil erosion rates. Soil erosion by wind

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Książki na temat "Wind tunnel"

Ajay, Kumar, Kegelman Jerome T, and United States. National Aeronautics and Space Administration., eds. The Langley wind tunnel enterprise. National Aeronautics and Space Administration, 1998.

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Ajay, Kumar, Kegelman Jerome T, and United States. National Aeronautics and Space Administration., eds. The Langley wind tunnel enterprise. National Aeronautics and Space Administration, 1998.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. AGARD, 1994.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Quality assessment for wind tunnel testing. AGARD, 1994.

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Hufnagel, Klaus. Wind Tunnel Balances. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-97766-5.

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Everhart, Joel L. Slotted-wall flow-field measurements in a transonic wind tunnel. Langley Research Center, 1991.

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B, Igoe William, Flechner Stuart G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Slotted-wall flow-field measurements in a transonic wind tunnel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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B, Igoe William, Flechner Stuart G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Slotted-wall flow-field measurements in a transonic wind tunnel. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

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E, Mineck Raymond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Adaptive wind tunnel walls: A selected, annotated bibliograpy. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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A, Kilgore Robert, Moore Deborah L, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Cryogenic wind tunnels: A comprehensive, annotated bibliography. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

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Części książek na temat "Wind tunnel"

Fujino, Yozo, Kichiro Kimura, and Hiroshi Tanaka. "Wind Tunnel Tests." In Wind Resistant Design of Bridges in Japan. Springer Japan, 2012. http://dx.doi.org/10.1007/978-4-431-54046-5_6.

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Schatzmann, Michael, Stylianos Rafailidis, and Nijs Jan Duijm. "Wind Tunnel Experiments." In Urban Air Pollution — European Aspects. Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-015-9080-8_14.

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Gao, Lei. "Wind Tunnel Test." In Encyclopedia of Ocean Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-10-6963-5_265-1.

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Gao, Lei. "Wind Tunnel Test." In Encyclopedia of Ocean Engineering. Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-10-6946-8_265.

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Bruno, Roberto, and Vincenzo Carbone. "A Natural Wind Tunnel." In Turbulence in the Solar Wind. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-43440-7_6.

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Matthews, R. K. "Hypersonic Wind Tunnel Testing." In Advances in Hypersonics. Birkhäuser Boston, 1992. http://dx.doi.org/10.1007/978-1-4612-0379-7_3.

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Fischer, Oliver. "Wind Tunnel Interference Effects." In Investigation of Correction Methods for Interference Effects in Open-Jet Wind Tunnels. Springer Fachmedien Wiesbaden, 2018. http://dx.doi.org/10.1007/978-3-658-21379-4_3.

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Zasso, Alberto, Alessandro Fontanella, and Marco Belloli. "3D Wind Tunnel Experiments." In Handbook of Wind Energy Aerodynamics. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-31307-4_31.

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Boorsma, Koen. "Wind Tunnel Rotor Measurements." In Handbook of Wind Energy Aerodynamics. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-31307-4_30.

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Boorsma, Koen. "Wind Tunnel Rotor Measurements." In Handbook of Wind Energy Aerodynamics. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-05455-7_30-2.

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Streszczenia konferencji na temat "Wind tunnel"

Gungor, Osman, Muhammed Kilic, Ayberk Caglar, and Ahmet Ezertas. "Wind Tunnel Testing of Heavy Class Attack Helicopter in a Pressurized Wind Tunnel." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1344.

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Heavy class attack helicopter development program aims to develop a new generation assault helicopter with high weapon capacity and modern combat technologies. Design requirements lead to a complicated aerodynamic shape. Wind tunnel tests gain importance for validation of aerodynamic design decisions and methodologies. A short test campaign is planned in a high Reynolds number environment which is achieved through pressurization. Generation of aerodynamic characteristics, effect of under-wing stores, effectivity of tail surfaces and main rotor hub interactions construct the base of test plan.

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Bringhurst, Katlynn, Scott Best, Vahid Nasr Esfahani, Victor Senft, Stuart Stevenson, and Felix Wittmeier. "CAATS – Automotive Wind Tunnel Calibrations." In WCX SAE World Congress Experience. SAE International, 2025. https://doi.org/10.4271/2025-01-8762.

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<div class="section abstract"><div class="htmlview paragraph">Wind tunnel calibration is necessary for repeatable and reproducible data for all industries interested in their output. Quantities such as wind speed, pressure gradients, static operating conditions, ground effects, force and moment measurements, as well as flow uniformity and angularity are all integral in an automotive wind tunnel’s data quality and can be controlled through appropriate calibration, maintenance, and statistical process control programs. The purpose of this technical paper is to (1) provide a basis of

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Scott, Robert C., Timothy Allen, Mark Castelluccio, et al. "Aeroservoelastic Wind-Tunnel Test of the SUGAR Truss Braced Wing Wind-Tunnel Model." In 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1172.

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Martin, Christopher A., Larry Jasmin, John S. Flanagan, Kari Appa, and Jayanth N. Kudva. "Smart wing wind tunnel model design." In Smart Structures and Materials '97, edited by Janet M. Sater. SPIE, 1997. http://dx.doi.org/10.1117/12.274675.

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Scherer, Lewis B., Christopher A. Martin, Kari Appa, Jayanth N. Kudva, and Mark N. West. "Smart wing wind tunnel test results." In Smart Structures and Materials '97, edited by Janet M. Sater. SPIE, 1997. http://dx.doi.org/10.1117/12.274694.

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Alves, Leonardo Boa Sorte, Marco Gabaldo, Luiz Severiano Dutra, and Jose Eduardo Mautone Barros. "Wind Tunnel Balance." In 26th SAE BRASIL Inernational Congress and Display. SAE International, 2017. http://dx.doi.org/10.4271/2017-36-0237.

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Dekterev, Ar A., A. A. Dekterev, and D. A. Dekterev. "PIXEL WIND TUNNEL." In XXXVIII Сибирский теплофизический семинар, посвященный 65-летию Института теплофизики им. С.С.Кутателадзе СО РАН. Сибирское отделение РАН, 2022. http://dx.doi.org/10.53954/9785604859551_73.

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"Wind Tunnel Methods." In SP-240: Performance-Based Design of Concrete Building for Wind Loads. American Concrete Institute, 2006. http://dx.doi.org/10.14359/18294.

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Burdett, Timothy A., and Kenneth W. Van Treuren. "Scaling Small-Scale Wind Turbines for Wind Tunnel Testing." In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-68359.

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Wind tunnel testing of wind turbines can provide valuable insights into wind turbine performance and provides a simple process to test and improve existing designs. However, the scale of most wind turbines is significantly larger than most existing wind tunnels, thus, the scaling required for testing in a typical wind tunnel presents multiple challenges. When wind turbines are scaled, often only geometric similarity and tip speed ratio matching are employed. Scaling in this manner can result in impractical rotational velocities. For wind tunnel tests that involve Reynolds numbers less than app

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Marks, Christopher R., Lauren Zientarski, Adam J. Culler, Benjamin Hagen, Brian M. Smyers, and James J. Joo. "Variable Camber Compliant Wing - Wind Tunnel Testing." In 23rd AIAA/AHS Adaptive Structures Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1051.

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Raporty organizacyjne na temat "Wind tunnel"

Slone, Scott, Marissa Torres, Alexander Stott, Ethan Thomas, and Robert Ibey. CRREL Environmental Wind Tunnel upgrades and the Snowstorm Library. Engineer Research and Development Center (U.S.), 2024. http://dx.doi.org/10.21079/11681/48077.

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Environmental wind tunnels are ideal for basic research and applied physical modeling of atmospheric conditions and turbulent wind flow. The Cold Regions Research and Engineering Laboratory's own Environmental Wind Tunnel (EWT)—an open-circuit suction wind tunnel—has been historically used for snowdrift modeling. Recently the EWT has gone through several upgrades, namely the three-axis chassis motors, variable frequency drive, and probe and data acquisition systems. The upgraded wind tunnel was used to simulate various snowstorm conditions to produce a library of images for training machine le

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Grossir, Guillaume. On the design of quiet hypersonic wind tunnels. Von Karman Institute for Fluid Dynamics, 2020. http://dx.doi.org/10.35294/tm57.

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This document presents a thorough literature review on the development of hypersonic quiet tunnels. The concept of boundary layer transition in high-speed flows is presented first. Its consequences on the free-stream turbulence levels in ground facilities are reviewed next, demonstrating that running boundary layers along the nozzle walls must remain laminar for quiet operation. The design key points that enable laminar boundary layers and hypersonic operation with low free-stream noise levels are then identified and discussed. The few quiet facilities currently operating through the world are

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Miles, Richard B., and Garry L. Brown. Radiatively Driven Hypersonic Wind Tunnel. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada403037.

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Mayda, Edward A., C. P. van Dam, David D. Chao, and Dale E. Berg. Flatback airfoil wind tunnel experiment. Office of Scientific and Technical Information (OSTI), 2008. http://dx.doi.org/10.2172/933221.

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Alexander, Michael G. Subsonic Wind Tunnel Testing Handbook. Defense Technical Information Center, 1991. http://dx.doi.org/10.21236/ada240263.

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Maniet, Edward R., and Jr. Wind Tunnel Measurements of Windscreen Performance. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada409180.

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Willard, Richard S., and Stan K. Kranzler. Improved Wind Tunnel Data Reduction Procedure. Defense Technical Information Center, 1996. http://dx.doi.org/10.21236/ada345019.

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Heim, E. R. CFD Wing/Pylon/Finned Store Mutual Interference Wind Tunnel Experiment. Defense Technical Information Center, 1991. http://dx.doi.org/10.21236/adb152669.

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Rahai, Hamid, Assma Begum, Jeremy Bonifacio, and Ryan Moffit. Experimental Investigations of Wind Shear from Passing a Vehicle. Mineta Transportation Institute, 2024. https://doi.org/10.31979/mti.2024.2334.

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Wind energy can be harnessed for various commercial and transportation-related applications. This study assessed experimentally the potential of capturing wind energy from the passage of vehicles for electric power generation. Both wind tunnel experiments and field tests were performed. The wind tunnel experiments were performed in an open-circuit low-speed wind tunnel at a free-stream mean velocity of 23 m/s. Five PVC pipes placed adjacent to the wind-blowing domain were used to simulate the columns under a freeway overpass. A scaled Ahmad body (simplified car body model) was used as the vehi

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Arunajatesan, Srinivasan, and Katya Casper. Trisonic Wind Tunnel (TWT )Complex Cavity Geometry. Office of Scientific and Technical Information (OSTI), 2015. http://dx.doi.org/10.2172/1177759.

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