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Relevant bibliographies by topics / Wind tunnel in Lanzhou University

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Academic literature on the topic 'Wind tunnel in Lanzhou University'

Author: Grafiati

Published: 4 June 2025

Last updated: 1 August 2025

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Journal articles on the topic "Wind tunnel in Lanzhou University"

1

Li, Shoutu, Ye Li, Congxin Yang, et al. "Design and Testing of a LUT Airfoil for Straight-Bladed Vertical Axis Wind Turbines." Applied Sciences 8, no. 11 (2018): 2266. http://dx.doi.org/10.3390/app8112266.

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The airfoil plays an important role in improving the performance of wind turbines. However, there is less research dedicated to the airfoils for Vertical Axis Wind Turbines (VAWTs) compared to the research on Horizontal Axis Wind Turbines (HAWTs). With the objective of maximizing the aerodynamic performance of the airfoil by optimizing its geometrical parameters and by considering the law of motion of VAWTs, a new airfoil, designated the LUT airfoil (Lanzhou University of Technology), was designed for lift-driven VAWTs by employing the sequential quadratic programming optimization method. Afte

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Ren, Wanmin, Qingsong Duan, Cunming Ma, Haili Liao, and Qiusheng Li. "Experimental investigation of the protective effect of wind barriers on high-speed railway bridge in inland strong wind area." Advances in Structural Engineering 22, no. 15 (2019): 3306–18. http://dx.doi.org/10.1177/1369433219862939.

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This study aims to investigate the wind protective effect of wind barriers on the Lanzhou–Xinjiang high-speed railway using wind tunnel tests. Wind barriers with different heights and porosities were analyzed. Two girders, that is, a box-girder and a trough-girder, each with 1:30 and 1:8 scales were experimentally investigated. The results suggest that the protective effect of the wind barrier with a height of 4 m and porosity of 20% is better than the others. The influence of wind barriers on the aerodynamic characteristics of train vehicles and girders must be analyzed simultaneously. The ae

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Shi, Long, Dongyuan Wang, Kai Cui, and Chunxiao Xue. "Comparative evaluation of concrete sand-control fences used for railway protection in strong wind areas." Railway Engineering Science 29, no. 2 (2021): 183–98. http://dx.doi.org/10.1007/s40534-020-00228-5.

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AbstractConcrete-plate fences have been widely adopted for windblown sand control and mitigation along railways. However, the inclination angles of inserting the concrete plate with respect to the vertical direction, i.e., straight or obliquely inserted concrete plates (SIP or OIP), significantly influence the efficiency of sand-control. This study performs a comparative evaluation of the SIP and OIP sand-control fences using wind tunnel testing and field monitoring data collected from the Lanzhou–Wulumuqi High-Speed Railway Project. The results show that the fence’s ability to reduce the wind

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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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Du, Meixia, Hai Zhu, Xiaochun Yin, et al. "Exploration of influenza incidence prediction model based on meteorological factors in Lanzhou, China, 2014–2017." PLOS ONE 17, no. 12 (2022): e0277045. http://dx.doi.org/10.1371/journal.pone.0277045.

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Humans are susceptible to influenza. The influenza virus spreads quickly and behave seasonally. The seasonality and spread of influenza are often associated with meteorological factors and have spatio-temporal differences. Based on the influenza cases and daily average meteorological factors in Lanzhou from 2014 to 2017, this study firstly aimed to analyze the characteristics of influenza incidence in Lanzhou and the impact of meteorological factors on influenza activities. Then, SARIMA(X) models for the prediction were established. The influenza cases in Lanzhou from 2014 to 2017 was more mal

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Čeheľová, Dagmara, Michal Franek, and Boris Bielek. "Atmospheric Boundary Layer Wind Tunnel of Slovak University of Technology in Bratislava." Applied Mechanics and Materials 887 (January 2019): 419–27. http://dx.doi.org/10.4028/www.scientific.net/amm.887.419.

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Aerodynamics is a relatively young scientific discipline, which started developing in the 50´s of last century. There are known several methods for calculating and measuring of the aerodynamic variables – in-situ measurements, wind tunnel measurements, CFD simulations and calculations according to national standards. Each method has its advantages and disadvantages. Nowadays a large focus is on experimental verifying the findings achieved with calculations help and CFD simulations. One of the verification possibilities are measurements in wind tunnels. The submitted paper deals with constructi

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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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Itō, H., R. Kobayashi, and Y. Kohama. "The low-turbulence wind tunnel at Tōhoku University." Aeronautical Journal 96, no. 954 (1992): 141–51. http://dx.doi.org/10.1017/s0001924000024738.

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SummaryA general-purpose low turbulence wind tunnel was constructed using the design method of Bradshaw. Sound absorbent material was used in every four corners to decrease sound intensity produced by a fan. The longitudinal component of turbulence intensity at the centre of the closed working section is less than 0.02% of the mean velocity in the speed range between 18 m/s arid 53 m/s. The mean velocity variations across the working section are within ±0.1% of the mean velocity.Performance measurements have been done at representative tunnel cross sections to clarify the behaviour of flow in

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Obreja, Dan. "Experimental techniques in the wind tunnel of naval architecture faculty." Analele Universităţii "Dunărea de Jos" din Galaţi Fascicula XI Construcţii navale/ Annals of "Dunărea de Jos" of Galati Fascicle XI Shipbuilding 44 (December 3, 2021): 5–10. http://dx.doi.org/10.35219/annugalshipbuilding/2021.44.01.

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The implementation of innovative solutions in the field of shipbuilding requires the continuous development of research infrastructure. The hydro-aerodynamic problems of fluid flow around the hulls can be solved with numerical and/or experimental techniques. In any case, the validation of the numerical solutions is performed in specialized hydro-aerodynamic laboratories by means of the experimental model tests. In this context, a wind tunnel was developed at the Naval Architecture Faculty of “Dunarea de Jos” University of Galati, in order to measure the aerodynamic forces and moments or the sp

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

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

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Dissertations / Theses on the topic "Wind tunnel in Lanzhou University"

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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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Bertholds, Alexander. "CFD Simulations of the New University of Sydney Boundary Layer Wind Tunnel." Thesis, Uppsala universitet, Institutionen för teknikvetenskaper, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-166945.

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Using Computational Fluid Dynamics Simulations, the flow in the new University of Sydney closed circuit wind tunnel has been analyzed prior to the construction of the tunnel. The objective was to obtain a uniform flow in the test section of the wind tunnel while keeping the pressure losses over the tunnel as low as possible. This was achieved by using several flow-improving components such as guide vanes, screens, a honeycomb and a settling chamber. The guide vanes were used in the corners and in the diverging part leading into the settling chamber, giving a significant improvement of the flow

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Himmerich, Peter. "SUPERSONIC CROSSFLOW VISUALIZATION USING THE UNIVERSITY OF CENTRAL FLORIDA SUPERSONIC WIND TUNNEL." Master's thesis, University of Central Florida, 2007. http://digital.library.ucf.edu/cdm/ref/collection/ETD/id/3553.

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The next generation air breathing engine that would enable an alternative to conventional air travel or suborbital flight is the supersonic ramjet engine (SCRAM) which requires a highly accelerated rate of fuel mixing and combustion. For this type of engine, one of the improvement opportunities lies in the injection of the fuel into the supersonic flow inside the combustor. In order to determine the flow field that develops when a sonic jet of secondary gas is injected into a supersonic free stream, a dedicated test section was developed which was attached to the existing supersonic wind tunne

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Whitacre, David L. "Development of an Icing Research Wind Tunnel at The University of Toledo." University of Toledo / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1376594446.

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Garcia, Jason S. "Design, Construction, and Characterization of the University of South Florida Wind Tunnel." Scholar Commons, 2018. https://scholarcommons.usf.edu/etd/7294.

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Much of the aerosol research completed at the University of South Florida has revolved around evaluating industrial hygiene equipment and instrumentation in environmental chambers. Data collected during these studies has provided valuable baseline data on equipment and instrument performance under calm air conditions. A newly constructed wind tunnel now allows researchers to evaluate industrial hygiene instruments under moving air conditions. Because the wind tunnel is capable of producing wind velocities that a worker could encounter in the occupational setting, researchers may gain insigh

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Goozee, Richard J. "Simulation of a complete shock tunnel using parallel computer codes /." St. Lucia, Qld, 2003. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe17470.pdf.

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Jeffries, Michael. "Initial investigations of transonic turbine aerodynamics using the Carleton University high-speed wind tunnel." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2001. http://www.collectionscanada.ca/obj/s4/f2/dsk3/ftp04/NQ60956.pdf.

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Okoro, Ndubuisi Emmanuel. "Development of a supersonic wind tunnel rapid real-time data acquisition and control system." Master's thesis, Mississippi State : Mississippi State University, 2005. http://sun.library.msstate.edu/ETD-db/ETD-browse/browse.

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Weiss, Julien. "Experimental determination of the free stream disturbance field in the short duration supersonic wind tunnel of Stuttgart University." [S.l. : s.n.], 2002. http://www.bsz-bw.de/cgi-bin/xvms.cgi?SWB10316296.

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Memon, Muhammad Omar. "Wingtip Vortices and Free Shear Layer Interaction in the Vicinity of Maximum Lift to Drag Ratio Lift Condition." University of Dayton / OhioLINK, 2017. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1492701624726378.

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Books on the topic "Wind tunnel in Lanzhou University"

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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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2

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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3

Sunyach, M. Performance of the high speed anechoic wind tunnel at Lyon University. National Aeronautics and Space Administration, 1986.

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4

Stock, David E. Wind tunnel study of fresh air inlet locations for Kennedy Library. Washington State University, 1995.

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5

Patrick, Moriarty, and United States. National Aeronautics and Space Administration., eds. Turbulence measurements on a flap-edge model: Final report : NASA-Ames University Consortium, NCC2-5140. National Aeronautics and Space Administration, 1998.

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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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7

Fisher, David. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. National Aeronautics and Space Administration, 1996.

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8

O, Thomas Flint, Nelson Robert C, and United States. National Aeronautics and Space Administration., eds. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. National Aeronautics and Space Administration, 1996.

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Fisher, David. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. National Aeronautics and Space Administration, 1996.

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O, Thomas Flint, Nelson Robert C, and United States. National Aeronautics and Space Administration., eds. Key topics for high-lift research: A joint wind tunnel/flight test approach : report for NASA-Ames University consortium, joint research interchange, May 1, 1995 - September 30, 1996. National Aeronautics and Space Administration, 1996.

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Book chapters on the topic "Wind tunnel in Lanzhou University"

1

Donovan, J. F., and M. S. Selig. "Low Reynolds Number Airfoil Design and Wind Tunnel Testing at Princeton University." In Lecture Notes in Engineering. Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-84010-4_4.

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2

Michelbach, Armin, and Reinhard Blumrich. "Upgrade of the full-scale aeroacoustic wind tunnel of Stuttgart University by FKFS." In Proceedings. Springer Fachmedien Wiesbaden, 2015. http://dx.doi.org/10.1007/978-3-658-08844-6_33.

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3

Aboelezz, Ahmed, Peter Makeen, and Hani Ghali. "Integrated Online Wind Tunnel Experiments and Assessment for Contingency Scenario: Case Study at the British University in Egypt (BUE)." In Advances in Intelligent Systems and Computing. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-67209-6_47.

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Bulut, Jane, Ferry Schrijer, and Bas van Oudheusden. "Oblique-Shock Wave Boundary Layer Interactions Control: Shock Control Bumps." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-86605-0_9.

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Abstract In this experimental study the effect of three-dimensional shock control bumps (SCB) on oblique shock wave/boundary layer interactions is investigated as a passive control method. It aims to develop an understanding of the effect of such devices on the interaction structure by means of studying the influence of the position of the bump with respect of the shock-impingement location, as well as the effect of the bump geometry (more in particular, the ramp section of the bump). The experiments were conducted in the ST-15 wind-tunnel at the Delft University of Technology for fully develo

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Missing, Timothy, and Holger Babinsky. "Unsteady Three-Dimensional Oblique Shock Wave Boundary-Layer Interactions." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-86605-0_8.

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Abstract Turbulent oblique Shock Wave Boundary Layer Interactions (SBLIs) were investigated experimentally in two rectangular test section blow down-type supersonic wind tunnels, to examine three-dimensionality induced by the presence of side-walls, as well as the low frequency separation bubble breathing oscillation. Testing was performed at Mach 2.5 and 2, with incident shock deflection angles of $$8^{\circ }$$ 8 ∘ and $$12^{\circ }$$ 12 ∘ at the Cambridge University (UCAM) and TU Delft (TUD) supersonic wind tunnel facilities respectively. In the UCAM facility, Conical shaped artificial corn

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Rehman, Fayyaz, Robert Benham, and Charlie Dunkel. "Design and the Development of an Anemometer Positioning System." In Advances in Transdisciplinary Engineering. IOS Press, 2023. http://dx.doi.org/10.3233/atde230927.

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Measurement of air flow through a fan is required during routine testing of several student projects using an existing two-metre-long wind tunnel at the University. Measurements of air velocity uses a handheld weather kit anemometer which is connected to a data logger. Inaccuracies in holding the equipment resulted in the basis of a project. This paper investigates and reviews the findings of the project, based on designing, prototyping, and evaluating a suitable system to hold the anemometer and allow positioning of it at any desired position within the cross-section of the wind tunnel. A rai

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Conference papers on the topic "Wind tunnel in Lanzhou University"

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Uppoor, Vivek, Howard Zheng, and Inderjit Chopra. "High Advance Ratio Wind Tunnel Testing of a Slowed Mach-scaled Rotor with Full-Wing and Trailing Propeller Lift and Thrust Compounding." In Vertical Flight Society 81st Annual Forum and Technology Display. The Vertical Flight Society, 2025. https://doi.org/10.4050/f-0081-2025-343.

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Wind tunnel tests and comprehensive rotorcraft analysis were carried out on a slowed main rotor full-wing lift and thrust-compounded helicopter with a trailing propeller to investigate the effects of rotor and wing configuration on performance, blade structural loads, and hub vibratory loads. Experiments were conducted at advance ratios up to 0.7, incorporating three full-wing configurations with symmetric and asymmetric incidence angles and three different rotor shaft tilt angles. Propulsive thrust was measured by a trailing pusher propeller with its own balance system. The wind tunnel test d

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Disotell, Kevin, Pourya Nikoueeyan, James Gregory, and Jonathan Naughton. "Single-Shot Pressure-Sensitive Paint Measurements of Static and Dynamic Stall on a Wind Turbine Airfoil." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10299.

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Results of a first application of pressure-sensitive paint (PSP) to a low Reynolds number wind turbine airfoil in static and dynamic stall are reported. Recognizing the need for global surface measurement techniques to resolve the unsteady three-dimensional loading on a moving wind turbine blade, fast-responding PSP was applied to the suction side of a Delft DU97-W-300 airfoil (maximum thickness-to-chord ratio of 30%) at a chord Reynolds number of 225,000 in the University of Wyoming open-return wind tunnel. Static and dynamic stall behaviors are compared using instantaneous and phase-averaged

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Lorber, Peter, Kyle Hird, Patrick Bowles, et al. "Compressible Dynamic Stall Alleviation Through High Momentum Blowing." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11375.

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An experiment was conducted in The Ohio State University Transonic Wind Tunnel on a high lift airfoil to evaluate the effectiveness of high momentum steady blowing for dynamic stall control. Computational fluid dynamics (CFD) was used to design airfoil modifications to tangentially inject air behind the leading edge. Extensive design, calibration, and post-test analysis efforts were required to achieve desired flow control system performance and data accuracy. Aerodynamic performance for steady and oscillatory angle-of-attack conditions was measured with the baseline smooth airfoil, with the s

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Schmaus, Joseph, and Inderjit Chopra. "Aeromechanics for a High Advance Ratio Coaxial Helicopter." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10162.

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A comprehensive analysis for evaluating performance and vibratory loads of a coaxial helicopter is developed, and some validations are carried out against existing experimental data. The methodology is extended from baseline UMARC to include interactional rotor wake between the coaxial rotors, modeling of relative phase between rotors and trim strategies for a coaxial helicopter. The simulation is used to define a flight envelope for an experimental rotor being developed by the University of Texas at Austin for testing in the Glenn L. Martin Wind Tunnel. Vertical hub loads and total rotor powe

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Reich, David, Rajiv Shenoy, Sven Schmitz, and Marilyn Smith. "An Assessment of the Long-Age Unsteady Rotor Hub Wake Physics for Empennage Analysis." In Vertical Flight Society 70th Annual Forum & Technology Display. The Vertical Flight Society, 2014. http://dx.doi.org/10.4050/f-0070-2014-9433.

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In addition to providing a comprehensive review and presentation of state-of-the-art experimental and computational efforts concerning rotor hub flows, this paper presents evidence that both experimental and computational capabilities are ready to foster the physical understanding of the long-age unsteady wake due to rotor hubs. A primary asset of this work is to demonstrate that two different rotor hub configurations show common characteristics of the underlying flow physics. The results of the Georgia Tech computations, when correlated with the experimental data from Penn State University, o

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Hammond, David. "Cranfield University Icing Wind Tunnel." In 41st Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-901.

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KOHAMA, Y., R. KOBAYASHI, and H. ITO. "Tohoku University low-turbulence wind tunnel." In 28th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3913.

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Künstner, Rudi, Jürgen Potthoff, and Ulf Essers. "The Aero-Acoustic Wind Tunnel of Stuttgart University." In International Congress & Exposition. SAE International, 1995. http://dx.doi.org/10.4271/950625.

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Bruckner, Adam P., Robert Blair, Shojiro Shindo, Scott Eberhardt, Carl Knowlen, and Sarah M. Musi. "The Kirsten Wind Tunnel at the University of Washington." In AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-0518.

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Nietzel, Kylar, Adrien Bouskela, Paul Dybskiy, Colby Thomas, and Sergey V. Shkarayev. "Wind Gust Simulation System Within Subsonic Wind Tunnel at the University of Arizona." In AIAA SCITECH 2025 Forum. American Institute of Aeronautics and Astronautics, 2025. https://doi.org/10.2514/6.2025-2358.

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