Relevant bibliographies by topics / Wind tunnel tests

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Wind tunnel tests'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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Journal articles on the topic "Wind tunnel tests"

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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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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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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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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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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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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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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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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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Dissertations / Theses on the topic "Wind tunnel tests"

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BACCHINI, ALESSANDRO. "Electric VTOL preliminary design and wind tunnel tests." Doctoral thesis, Politecnico di Torino, 2020. http://hdl.handle.net/11583/2847140.

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Frison, Giovanni. "Aeroelastic and aerodynamic wind tunnel tests for tall buildings." Doctoral thesis, Università degli studi di Padova, 2019. http://hdl.handle.net/11577/3423186.

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Starting from the consolidated concept of aerodynamic model, a benchmark is proposed to further asses an extend its capability of correctly identify the dynamic response of a tall building, devoting particular attention to the contribution of higher-order modes and the possible presence of aerodynamic damping. Being the extrema ratio in terms of accuracy and reliability, a full-aeroelastic model of a tall building is presented as the subject of comparison. The complexity involved in the dynamic wind-tunnel scaling led to the definition of a novel semi-automatized procedure. Based on the author
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Warsido, Workamaw Paulos. "Reducing Uncertainties in Estimation of Wind Effects on Tall Buildings Using Aerodynamic Wind Tunnel Tests." FIU Digital Commons, 2013. http://digitalcommons.fiu.edu/etd/939.

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Tall buildings are wind-sensitive structures and could experience high wind-induced effects. Aerodynamic boundary layer wind tunnel testing has been the most commonly used method for estimating wind effects on tall buildings. Design wind effects on tall buildings are estimated through analytical processing of the data obtained from aerodynamic wind tunnel tests. Even though it is widely agreed that the data obtained from wind tunnel testing is fairly reliable the post-test analytical procedures are still argued to have remarkable uncertainties. This research work attempted to assess the uncert
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Meszaros, Steven P. "Wind tunnel tests to determine effective leakage area in model grain bins." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk2/tape17/PQDD_0001/MQ32189.pdf.

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Lehmkuehler, Kai. "A Direct Comparison of Small Aircraft Dynamics between Wind Tunnel and Flight Tests." Thesis, The University of Sydney, 2016. http://hdl.handle.net/2123/16511.

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The miniaturization of embedded electronics and sensors driven by the rapid development of mobile devices has enabled powerful avionics systems for very small aircraft. This enables a potential step forward in accurate flight data gathering for vehicles weighing 5 kg or less. Being able to flight test a small platform like this also allows the comparison of the results with reference data from ground testing in a standard sized wind tunnel of an identical airframe. With this process, the following questions can be answered: Firstly, would such a system then be able to collect accurate flight d
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Kusmarwanto, I. "Ground effect on a rotor wake." Thesis, Cranfield University, 1985. http://dspace.lib.cranfield.ac.uk/handle/1826/4545.

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The effect of the ground on a rotor wake in forward flight has been investigated experimentally in the working section of an 8ft x Oft straight-through wind tunnel. A three bladed fully articulated rotor with a solidity ratio of 0.07 and diameter of 1.06m, powered by a hydraulic motor, has been tested at a height of 0.47 rotor diameter above a solid ground board which has an elliptical leading edge. Tests have been run at various low advance ratios (<0.1) with two collective pitch settings. A three-element hot wire anemometer probe has been used to measure the average value of the three compon
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Breton, Simon-Philippe. "Study of the stall delay phenomenon and of wind turbine blade dynamics using numerical approaches and NREL’s wind tunnel tests." Doctoral thesis, Norwegian University of Science and Technology, Department of Civil and Transport Engineering, 2008. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-2275.

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Mesrobian, Chris Eden. "Concept Study of a High-Speed, Vertical Take-Off and Landing Aircraft." Thesis, Virginia Tech, 2009. http://hdl.handle.net/10919/35574.

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The purpose of the study was to evaluate the merits of the DiscRotor concept that combine the features of a retractable rotor system for vertical take-off and landing (VTOL) with an integral, circular wing for high-speed flight. Tests were conducted to generate basic aerodynamic characteristics of the DiscRotor in hover and in fixed-wing flight. <p> To assess the DiscRotor during hover, small scale tests were conducted on a 3ft diameter rotor without the presence of a fuselage. A â hover rigâ was constructed capable of rotating the model rotor at speeds up to 3,500 RPM to reach tip speeds
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de, Laval Jonathan. "Simulation of thermal tests in the climatic wind tunnel CD7 at Scania Master thesis project in fluid mechanics." Thesis, KTH, Mekanik, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-195726.

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The Swedish truck and bus manufacturer Scania has a number of test facilities to support the R&amp;D department and for verification of vehicle properties. The latest addition is the climatic wind tunnel Chassis Dynamometer 7 (CD7) which can fit trucks and buses for full scale testing and maintain temperatures in the range from -35 to 50 degree Celsius in the flow circuit, furthermore it can generate both rain and snow conditions. This means that vehicles can be tested in a controlled and repeatable manner at many critical driving conditions. However, since CD7 is a new facility there is a nee
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Schouten, Shane Michael. "Complete CFD analysis of a Velocity XL-5 RG with flight-test verification." Texas A&M University, 2008. http://hdl.handle.net/1969.1/85894.

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The Texas A&M Flight Research Laboratory (FRL) recently received delivery of its newest aircraft, the Velocity XL-5 RG. The Velocity can fly faster than the other aircraft owned by the FRL and does not have a propeller in the front of the aircraft to disrupt the air flow. These are definite advantages that make the Velocity an attractive addition to the FRL inventory to be used in boundary-layer stability and transition control. Possible mounting locations built into the aircraft for future projects include hard points in the wings and roof of the fuselage. One of the drawbacks of the aircraft
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Books on the topic "Wind tunnel tests"

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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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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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MacKinnon, A. Wind tunnel tests on a variable camber wing. College of Aeronautics, Cranfield University, 1993.

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Galway, R. D. The IAR High Reynolds Number Two-Dimensional Test Facility - a description of equipment and procedures common to most 2-D airfoil tests. National Research Council Canada, Institute for Aerospace Research, 1990.

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Galway, R. D. The IAR high Reynolds number two-dimensional test facility - a description of equipment and procedures common to most 2-D airfoil tests. National Research Council of Canada, Institute for Aerospace Research, 1990.

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Center, Lewis Research, and United States. National Aeronautics and Space Administration., eds. Flow field surveys of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1993 test). National Aeronautics and Space Administration, Lewis Research Center, 1998.

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Kelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. National Aeronautics and Space Administration, Langley Research Center, 1994.

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Kelly, Abeyounis William, and Langley Research Center, eds. 16-foot transonic tunnel test section flowfield survey. National Aeronautics and Space Administration, Langley Research Center, 1994.

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Book chapters on the topic "Wind tunnel tests"

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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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Gibertini, G., D. Grassi, N. Scarpellini, D. Spreafico, and D. Trovato. "Wind Tunnel Tests of Speed-Skier." In IFMBE Proceedings. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-14515-5_58.

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Nicolosi, F., V. Cusati, D. Ciliberti, Pierluigi Della Vecchia, and S. Corcione. "Aeroelastic Wind Tunnel Tests of the RIBES Wing Model." In Flexible Engineering Toward Green Aircraft. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-36514-1_2.

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Starossek, U., H. Ziems, and T. Ferenczi. "Eccentric-wing flutter stabilizer: Analysis and wind tunnel tests." In Insights and Innovations in Structural Engineering, Mechanics and Computation. CRC Press, 2016. http://dx.doi.org/10.1201/9781315641645-9.

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Zhu, Weijun, and Dichen Li. "Overview of Wind Tunnel Test Models." In Models for Wind Tunnel Tests Based on Additive Manufacturing Technology. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-5877-1_1.

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Zhu, Weijun, and Dichen Li. "Inspection Techniques of Wind Tunnel Test Models Based on Additive Manufacturing Wind Tunnel Test Models." In Models for Wind Tunnel Tests Based on Additive Manufacturing Technology. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-5877-1_4.

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Matejka, Milan. "Experimental Results of Synthetic Jet Wind Tunnel Tests." In Recent Progress in Flow Control for Practical Flows. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-50568-8_13.

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Kirchheck, Daniel, Dominik Saile, and Ali Gülhan. "Rocket Wake Flow Interaction Testing in the Hot Plume Testing Facility (HPTF) Cologne." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_9.

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Abstract Rocket wake flows were under investigation within the Collaborative Research Centre SFB/TRR40 since the year 2009. The current paper summarizes the work conducted during its third and final funding period from 2017 to 2020. During that phase, focus was laid on establishing a new test environment at the German Aerospace Center (DLR) Cologne in order to improve the similarity of experimental rocket wake flow–jet interaction testing by utilizing hydrogen–oxygen combustion implemented into the wind tunnel model. The new facility was characterized during tests with the rocket combustor mod
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Schito, P., I. Bayati, M. Belloli, L. Bernini, V. Dossena, and A. Zasso. "Numerical Wind Tunnel Tests of an Open Data IPC-VAWT." In Wind Energy Exploitation in Urban Environment. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-74944-0_8.

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Sergei, Solovev, and Khrapunov Evgenii. "Improving the Aerodynamic Stability of Bridges. Wind Tunnel Tests." In Structural Integrity. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-29227-0_54.

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Conference papers on the topic "Wind tunnel tests"

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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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Stabellini, Alessandro, Iwan Philipsen, Joost Hakkaart, et al. "First NICETRIP Powered Wind Tunnel Tests Successfully Completed in DNW-LLF." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9660.

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A team of European Industry and academic researchers led by AgustaWestland, a Finmeccanica company, have successfully completed wind tunnel tests of a 1/5th scale model of a tiltwing/tiltrotor aircraft called ERICA (Enhanced Rotorcraft Innovative Concept Achievement) at the DNW-LLF wind tunnel (German-Dutch Wind Tunnels Large Low-speed Facility) in July 2013. This intensive research is partially funded by the European Commission under an EU sixth framework programme called NICETRIP (Novel Innovative Competitive Effective Tilt Rotor Integrated Project). As part of the NICETRIP programme, a 1/5t
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Raz, Reuben, Marcos Berrios, Luigi Cicolani, Omer Fogel, and Aviv Rosen. "Using Wind Tunnel Tests to Investigate Dual Lift Trim, Maneuvers, Stability and Control." In Vertical Flight Society 73rd Annual Forum & Technology Display. The Vertical Flight Society, 2017. http://dx.doi.org/10.4050/f-0073-2017-12186.

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The paper presents results of wind tunnel tests of a pendant dual lift system. A rig has been designed and built to represent the helicopter hooks and the suspension and load below the hooks. Four of the six degrees of freedom of movement of the hooks are modeled and the hooks are operated by open or closed loop control systems. At first quasi-steady maneuvering is studied. A special analytic model is derived and then used to study a typical maneuver and system sensitivities to servo inputs and drag estimation errors. A good agreement is shown between analytic and test results. Then a nonlinea
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Coetzee, Etienne, Mark H. Lowenberg, and Simon A. Neild. "Flexible High Aspect Ratio Wing Wind Tunnel Tests." In AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-1311.

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Schottler, Jannik, Agnieszka Hölling, Joachim Peinke, and Michael Hölling. "Wind tunnel tests on controllable model wind turbines in yaw." In 34th Wind Energy Symposium. American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-1523.

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Oerlemans, Stefan, and Paul Migliore. "Aeroacoustic Wind Tunnel Tests of Wind Turbine Airfoils." In 10th AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-3042.

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Plourde, B. D., J. P. Abraham, G. S. Mowry, and W. J. Minkowycz. "Wind-Tunnel Tests of Vertical-Axis Wind Turbine Blades." In ASME 2011 5th International Conference on Energy Sustainability. ASMEDC, 2011. http://dx.doi.org/10.1115/es2011-54604.

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An ongoing research project is investigating the potential of locating vertical-axis wind turbines (WT) on remote, off-grid cellular communication towers. The goal of the WT is to provide local power generation to meet the electrical needs of the tower. While vertical-axis devices are less efficient than their more traditional horizontal-axis counterparts, they provide a number of practical advantages which make them a suitable choice for the present situation. First, the direction of their axis is aligned with the existing tower and its rotation does not interfere with the tower structure. Se
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"MORPHING WING REAL TIME OPTIMIZATION IN WIND TUNNEL TESTS." In 7th International Conference on Informatics in Control, Automation and Robotics. SciTePress - Science and and Technology Publications, 2010. http://dx.doi.org/10.5220/0002885701140124.

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Corneille, Jennifer, and M. Franke. "Wind tunnel tests of a joined wing missile model." In 38th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-938.

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Vnuchkov, D. A., V. I. Zvegintsev, D. G. Nalivaychenko, V. I. Smoljaga, and A. V. Stepanov. "Solid fuel ramjet tests in wind tunnel." In INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2018). Author(s), 2018. http://dx.doi.org/10.1063/1.5065090.

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Reports on the topic "Wind tunnel tests"

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Ghee, Terence A., and Nigel J. Taylor. Low-Speed Wind Tunnel Tests on a Diamond Wing High Lift Configuration. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada377908.

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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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Hosoya, N., J. A. Peterka, R. C. Gee, and D. Kearney. Wind Tunnel Tests of Parabolic Trough Solar Collectors: March 2001--August 2003. Office of Scientific and Technical Information (OSTI), 2008. http://dx.doi.org/10.2172/929597.

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Sitek, M. A., and S. A. Lottes. CFD Simulations of Wind Tunnel Tests On Deer Isle – Sedgwick Bridge Model. Part 1. Static tests. Office of Scientific and Technical Information (OSTI), 2018. http://dx.doi.org/10.2172/1433491.

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Gillard, William J. Innovative Control Effectors (Configuration 101) Dynamic Wind Tunnel Test Report. Rotary Balance and Forced Oscillation Tests. Defense Technical Information Center, 1998. http://dx.doi.org/10.21236/ada362903.

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Abdel-Fattah, A. M., and Y. Y. Link. Wind Tunnel Tests on Jindivik Air Intake Duct with and Without an Auxiliary Intake. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada251676.

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Ligotke, M. W., G. W. Dennis, and L. L. Bushaw. Wind tunnel tests of biodegradable fugitive dust suppressants being considered to reduce soil erosion by wind at radioactive waste construction sites. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/10190697.

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Selig, M. S., and B. D. McGranahan. Wind Tunnel Aerodynamic Tests of Six Airfoils for Use on Small Wind Turbines; Period of Performance: October 31, 2002--January 31, 2003. Office of Scientific and Technical Information (OSTI), 2004. http://dx.doi.org/10.2172/15007930.

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Oerlemans, S. Wind Tunnel Aeroacoustic Tests of Six Airfoils for Use on Small Wind Turbines; Period of Performance: August 23, 2002 through March 31, 2004. Office of Scientific and Technical Information (OSTI), 2004. http://dx.doi.org/10.2172/15007773.

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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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Abstract:
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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