Relevant bibliographies by topics / Wind tunnel testing

Contents

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

Academic literature on the topic 'Wind tunnel testing'

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

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Journal articles on the topic "Wind tunnel testing"

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Shindo, Shojiro. "Wind Tunnel Testing." Journal of the Visualization Society of Japan 15, Supplement1 (1995): 277–80. http://dx.doi.org/10.3154/jvs.15.supplement1_277.

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Hasan, Inamul, R. Mukesh, P. Radha Krishnan, R. Srinath, Dhanya Prakash Babu, and Negash Lemma Gurmu. "Wind Tunnel Testing and Validation of Helicopter Rotor Blades Using Additive Manufacturing." Advances in Materials Science and Engineering 2022 (September 21, 2022): 1–13. http://dx.doi.org/10.1155/2022/4052208.

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This research paper aims to validate the aerodynamic performance of rotor blades using additive manufacturing techniques. Wind tunnel testing is a technique used to find the flow characteristics of the body. Computational fluid dynamics (CFD) techniques are used for aerodynamic analysis, and validation should be done using wind tunnel testing. In the aerodynamic testing of models, additive manufacturing techniques help in validating the results by making models easily for wind tunnels. Recent developments in additive manufacturing help in the aerodynamic testing of models in wind tunnels. The
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Zhang, Zheng Yu, Xu Hui Huang, Jiang Yin, and Han Xuan Lai. "Videogrammetric Techniques for Wind Tunnel Testing and Applications." Advanced Materials Research 986-987 (July 2014): 1629–33. http://dx.doi.org/10.4028/www.scientific.net/amr.986-987.1629.

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Videogrammetric measurement is a research focus for the organizations of wind tunnel test because of its no special requirements on the test model, its key techniques for the vibration environment of the high speed wind tunnel are introduced by this paper, such as the solution of exterior parameters with big-angle large overlap, the algorithm of image processing for extracting marked point, the method of camera calibration and wave-front distortion field measurement. The great requirements and application prospects of videogrammetry in wind tunnel fine testing have been demonstrated by several
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Lara, Andrés, Jonathan Toledo, and Robert Paul Salazar Romero. "Characterization, Design Testing and Numerical Modeling of a Subsonic-Low Speed Wind Tunnel." Ingeniería 27, no. 1 (2022): e17973. http://dx.doi.org/10.14483/23448393.17973.

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Context: Wind tunnels are essential devices in the study of flow properties through objects and scaled prototypes. This work presents a numerical study to characterize an existing wind tunnel, proposing modifications with the aim to improve the quality of the flow in the test chamber. Method: Experimental measurements of the inlet velocity and pressure distribution of a wind tunnel are nperformed. These empirical values are used as parameters to define boundary conditions in simulations. The Finite Element Method (FEM) at low speeds is implemented to determine the stream function by using a st
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Stalker, R. J. "Modern developments in hypersonic wind tunnels." Aeronautical Journal 110, no. 1103 (2006): 21–39. http://dx.doi.org/10.1017/s0001924000004346.

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AbstractThe development of new methods of producing hypersonic wind-tunnel flows at increasing velocities during the last few decades is reviewed with attention to airbreathing propulsion, hypervelocity aerodynamics and superorbital aerodynamics. The role of chemical reactions in these flows leads to use of a binary scaling simulation parameter, which can be related to the Reynolds number, and which demands that smaller wind tunnels require higher reservoir pressure levels for simulation of flight phenomena. The use of combustion heated vitiated wind tunnels for propulsive research is discusse
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Shahidin, Haziq Idraki, Mohd Rosdzimin Abdul Rahman, Azam Che Idris, and Mohd Rashdan Saad. "3D Printed Models vs Conventional Models: Comparison of Aerodynamic Performance for Wind Tunnel Experiments." Jurnal Kejuruteraan si4, no. 2 (2021): 101–4. http://dx.doi.org/10.17576/jkukm-2021-si4(2)-15.

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Traditionally, wind tunnel models are made of metal and the processes are very expensive. Since then, many researchers have been looking for new alternatives, hence 3D printing technology is the solution. Under right test conditions, 3D printed parts could be tested in a wind tunnel to get the aerodynamic performances. By using 3D printing technology, the cost and time can be significantly reduced to produce the wind tunnel models. This investigation was done to compare the aerodynamic performances which are drag and lift forces of the existing wind tunnel metal models with 3D printed wind tun
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Greenwell, D. I. "Transonic industrial wind tunnel testing in the 2020s." Aeronautical Journal 126, no. 1295 (2021): 125–51. http://dx.doi.org/10.1017/aer.2021.107.

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AbstractWind tunnels remain an essential element in the design and development of flight vehicles. However, graduates in aerospace engineering tend to have had little exposure to the demands of industrial experimental work, particularly at high speed, a situation exacerbated by a lack of up-to-date reference material. In an attempt to fill this gap, this paper presents an overview of the current and near-term status and usage of transonic industrial wind tunnels. The review is aimed at recent entrants to the field, with the aim of helping them make the step from research projects in small univ
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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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Daneshmand, Saeed, Cyrus Aghanajafi, and Hossein Shahverdi. "Investigation of rapid manufacturing technology with ABS material for wind tunnel models fabrication." Journal of Polymer Engineering 32, no. 8-9 (2012): 575–84. http://dx.doi.org/10.1515/polyeng-2012-0089.

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Abstract Nowadays, several procedures are used for manufacturing wind tunnel models. These methods include machining, casting, molding and rapid prototyping. Raw materials such as metals, ceramics, composites and plastics are used in making these models. Dimension accuracy, surface roughness and material strength are significant parameters which are effective in wind tunnel manufacturing and testing. Wind tunnel testing may need several models. Traditional methods for constructing these models are both costly and time consuming. In this research, a study has been undertaken to determine the su
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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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Dissertations / Theses on the topic "Wind tunnel testing"

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Abrahamsen, Ida Sinnes. "Wind tunnel model testing of offshore platforms." Thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for energi- og prosessteknikk, 2012. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-18627.

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The purpose of this thesis is to highlight some of the areas of interest when it comes to wind tunnel experimenting of offshore platforms regarding stability concerns such as critical angles and wind overturning moment. Some important factors include design of tower geometry, the effect of surface roughness on drag, methods of calculating blockage corrections of wall interference and the generation of an atmospheric boundary layer to resemble full-scale conditions. Data obtained from wind tunnel experiments with two different models have been compared and discussed according to the areas of in
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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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Kayisoglu, Bengi. "Investigation Of Wind Effects On Tall Buildings Through Wind Tunnel Testing." Master's thesis, METU, 2011. http://etd.lib.metu.edu.tr/upload/12613324/index.pdf.

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In recent years, especially in the crowded city-centers where land prizes have become extremely high, tall buildings with more than 30 floors have started to be designed and constructed in Turkey. On the other hand, the technical improvements have provided the opportunity of design and construction of more slender structures which are influenced by the wind actions more. If the building is flexible, wind can interact with it so the wind induced oscillations can be significantly magnified. In order to analyze the response of such buildings under wind effects, wind tunnel tests are accepted to b
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Sheng, Wanan. "CFD simulations in support of wind tunnel testing." Thesis, University of Glasgow, 2003. http://theses.gla.ac.uk/5393/.

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CFD and wind tunnel simulations are complementary due to their inherent limitations. Wind tunnel tests apply to any hypothesis, but are limited by the tunnel wall interference/blockage, the model details, and even the distortion of the model. CFD are not limited in any of these ways, but limited in speed and memory and the lack of determinate set of equations. Theoretically, CFD can provide an assessment of any problem in fluid dynamics (Direct Numerical Simulation), but the requirements of speed and memory are far from being met presently, or even in the foreseeable future. Of necessity, pres
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Abudaram, Yaakov Jack. "Wind tunnel testing of load-alleviating membrane wings." [Gainesville, Fla.] : University of Florida, 2009. http://purl.fcla.edu/fcla/etd/UFE0041340.

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Hameury, Michel. "Development of the tolerant wind tunnel for bluff body testing." Thesis, University of British Columbia, 1987. http://hdl.handle.net/2429/27311.

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In conventional wind tunnels the solid-wall or open-jet test section imposes on the flow field around the test model new boundary conditions absent in free air. Unless a small model is used, the solid-wall test section generally increases the loadings on the model while the open-jet boundary decreases the loadings compared to the unconfined case. However, the development of a low wall-interference test section and its successful demonstration would allow the testing of relatively large models without the application of often uncertain correction formulae. The Tolerant wind tunnel, which makes
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Kong, Lingzhe. "Experimental investigation of the tolerant wind tunnel for unsteady airfoil motion testing." Thesis, University of British Columbia, 1991. http://hdl.handle.net/2429/29992.

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Previously, the concept of the tolerant wind tunnel, developed in the Department of Mechanical Engineering, U. B. C., was tested only for stationary models. In the present study, the concept is investigated for unsteady airfoil motion. The new wind tunnel test section, using the opposite effects of solid and open boundaries, is a new approach to reduce wall blockage effects. Consisting of vertical airfoil slats uniformly spaced on both side walls in the test section, it is designed to produce a nearly free-air test environment for the test model, which leads to negligible or small corrections
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Hetherington, Ben. "Interference of supports used for ground vehicle wind tunnel testing." Thesis, Durham University, 2006. http://etheses.dur.ac.uk/2671/.

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In order to provide a correct aerodynamic simulation of a vehicle travelling along the ground, models are tested using rotating wheels in a wind tunnel with a moving ground. In the most common of moving ground configurations the model is supported by an overhead strut, usually designed as an aerofoil profile to minimise interference, with the wheels supported by lateral stings hinged to mounts outside the span of the moving ground plane. ๒ using this type of configuration it is assumed that the presence of the intruding supports do not markedly affect the aerodynamic behaviour of the model, bu
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Lewis, Mark Charles. "Aerofoil testing in a self-streamlining flexible walled wind tunnel." Thesis, University of Southampton, 1987. https://eprints.soton.ac.uk/52285/.

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Ratliff, Card. "Revitalization and initial testing of a blowdown supersonic wind tunnel." Master's thesis, Mississippi State : Mississippi State University, 2008. http://library.msstate.edu/etd/show.asp?etd=etd-07312008-093307.

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Books on the topic "Wind tunnel testing"

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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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American Institute of Aeronautics and Astronautics., ed. Recommended practice: Wind tunnel testing. American Institute of Aeronautics and Astronautics, 2003.

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Barlow, Jewel B. Low-speed wind tunnel testing. 3rd ed. Wiley, 1999.

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United States. National Aeronautics and Space Administration., ed. Wind tunnel testing and research. National Aeronautics and Space Administration, 1994.

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Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel., ed. Quality assessment for wind tunnel testing. Agard, 1994.

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Center, Langley Research, and United States. National Aeronautics and Space Administration, eds. Aeroservoelastic testing of free flying wind tunnel models. National Aeronautics and Space Administration, Langley Research Center, 2013.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., ed. The status of two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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American Society of Civil Engineers. Wind tunnel testing for buildings and other structures. American Society of Civil Engineers, 2012.

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Book chapters on the topic "Wind tunnel testing"

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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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Mora, R. Bardera. "Unmanned Aircraft Wind Tunnel Testing." In Advanced UAV Aerodynamics, Flight Stability and Control. John Wiley & Sons, Ltd, 2017. http://dx.doi.org/10.1002/9781118928691.ch5.

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Brownlie, Len W. "Wind Tunnels: Design Considerations in Wind Tunnel Testing of Cyclists." In Biomechanical Principles and Applications in Sports. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-13467-9_4.

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Bottasso, Carlo L., and Filippo Campagnolo. "Wind Tunnel Testing of Wind Turbines and Farms." In Handbook of Wind Energy Aerodynamics. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-31307-4_54.

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Bottasso, Carlo L., and Filippo Campagnolo. "Wind Tunnel Testing of Wind Turbines and Farms." In Handbook of Wind Energy Aerodynamics. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-05455-7_54-1.

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Gibertini, G., G. Campanardi, L. Guercilena, and C. Macchi. "Cycling Aerodynamics: Wind Tunnel Testing versus Track Testing." In IFMBE Proceedings. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-14515-5_3.

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Yinzhi, He, Zhigang Yang, and Yigang Wang. "Wind Noise Testing at Shanghai Automotive Wind Tunnel Center." In Lecture Notes in Electrical Engineering. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-33832-8_44.

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He, Yinzhi, Z. Yang, and Y. Wang. "Wind noise testing at the full scale aeroacoustic wind tunnel of Shanghai Automotive Wind Tunnel Center." In Proceedings. Springer Fachmedien Wiesbaden, 2014. http://dx.doi.org/10.1007/978-3-658-05130-3_97.

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Chazot, Olivier. "Aerospace Flight Modeling and Experimental Testing." In Uncertainty in Engineering. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-83640-5_9.

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AbstractValidation processes for aerospace flight modeling require to articulate uncertainty quantification methods with the experimental approach. On this note, the specific strategies for the reproduction of re-entry flow conditions in ground-based facilities are reviewed. It shows how it combines high-speed flow physics with the hypersonic wind tunnel capabilities.
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Sears, W. R. "A Wind-Tunnel Method for V/STOL Testing." In Recent Advances in Aerodynamics. Springer New York, 1986. http://dx.doi.org/10.1007/978-1-4612-4972-6_14.

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Conference papers on the topic "Wind tunnel testing"

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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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Karli, Geoffrey, Sihong Yan, and Jose Palacios. "Full-Scale EVTOL Rotor Icing Wind Tunnel Testing." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-0034.

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In recent years, the electrically powered Urban Air Mobility (UAM) market has witnessed significant growth, fueled by advances in electric motor and high-power-density lithium battery technologies. This surge of interest has prompted an exploration into the design and functionality of electric vertical take-off and landing (eVTOL) vehicles, particularly those with multi-tilt-rotor configurations. These eVTOL vehicles, capable of operating at higher RPMs than traditional helicopters, face unique challenges, especially under adverse environmental conditions such as icing. Aircraft airframe icing
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BARNWELL, R., C. EDWARDS, R. KILGORE, and D. DRESS. "Optimum transonic wind tunnel." In 14th Aerodynamic Testing Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-755.

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BUSHNELL, D., and R. TRIPI. "Supersonic wind tunnel optimization." In 14th Aerodynamic Testing Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-773.

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Schoenfeld, William, and Francis Priolo. "Automated wind tunnel testing." In 36th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-709.

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TRIMMER, L., A. CARY, JR., and R. VOISINET. "The optimum hypersonic wind tunnel." In 14th Aerodynamic Testing Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-739.

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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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Ozkan, Ender, Emanuele Mattiello, Francesco Dorigatti, et al. "Sazlidere Bridge Wind Tunnel Testing Assisted Design." In IABSE Symposium, Istanbul 2023: Long Span Bridges. International Association for Bridge and Structural Engineering (IABSE), 2023. http://dx.doi.org/10.2749/istanbul.2023.0936.

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<p>In the context of the Northern Marmara Motorway Section 8 Project, a new cable-stayed bridge, the Sazlidere Bridge, is being designed and works have already started on site. To support this fast-paced project, RWDI is collaborating with the design team and providing wind engineering services. The activities employ wind tunnel experiments and are focused on two main aspects: aerodynamic stability of the bridge and the risk of wind-induced overturning of large lorries crossing the bridge. With respect to aerodynamic stability, limited tests on a sectional model of the bridge deck were p
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SCAGGS, NORMAN, RICHARD NEUMANN, and ANTHONY LAGANELLI. "Hypersonic wind tunnel nozzle study." In 17th Aerospace Ground Testing Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-4012.

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Reports on the topic "Wind tunnel testing"

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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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Butterfield, C. P., W. P. Musial, and D. A. Simms. Combined Experiment Phase 1. [Horizontal axis wind turbines: wind tunnel testing versus field testing]. Office of Scientific and Technical Information (OSTI), 1992. http://dx.doi.org/10.2172/6882369.

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Ruyten, Wim. Toward an Integrated Optical Data System for Wind Tunnel Testing. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada370964.

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Simms, D., S. Schreck, M. Hand, et al. Plans for Testing the NREL Unsteady Aerodynamics Experiment 10m Diameter HAWT in the NASA Ames Wind Tunnel: Minutes, Conclusions, and Revised Text Matrix from the 1st Science Panel Meeting. Office of Scientific and Technical Information (OSTI), 2000. http://dx.doi.org/10.2172/763620.

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Wagner, Matthew J., and Gary A. Dale. The Design and Testing of Pneumatic Systems for Measuring Low Pressures in Hypersonic Wind Tunnels. Defense Technical Information Center, 1985. http://dx.doi.org/10.21236/ada379715.

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Hill, David W., Carman Jr., and Jr Jack B. User Requirements and Information for Captive Trajectory and Grid Testing in the PWT Aerodynamic Wind Tunnels (4T/16T/16S). Defense Technical Information Center, 1985. http://dx.doi.org/10.21236/ada334792.

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