Relevant bibliographies by topics / Wind-pressure Measurement

Contents

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

Academic literature on the topic 'Wind-pressure Measurement'

Author: Grafiati
Published: 10 December 2022
Last updated: 31 July 2025

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Journal articles on the topic "Wind-pressure Measurement"

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Liang, Shu Guo, Xiao Hui Peng, and Lei Wang. "Comparative Study between Field Measurement and Wind Tunnel Test of Wind Pressure on Wuhan International Stock Building." Applied Mechanics and Materials 590 (June 2014): 341–48. http://dx.doi.org/10.4028/www.scientific.net/amm.590.341.

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Field measurement and wind tunnel test of wind pressure on the surfaces of Wuhan International Stock Building were carried out in this paper, and the mean wind pressure coefficients, RMS wind pressure coefficients, wind pressure spectra as well as coherence functions were discussed. Meanwhile wind pressure distributions were analyzed. The results demonstrated that the distribution of the surface mean wind pressure coefficients obtained by wind tunnel test approximately agreed with that by field measurement, especially the mean wind pressure coefficients on the windward obtained by the wind tun
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Kolbe, Sven, Manuel Mohr, Martin Maier, Laurin Osterholt, Barry Gardiner, and Dirk Schindler. "On the Potential of Using Air Pressure Fluctuations to Estimate Wind-Induced Tree Motion in a Planted Scots Pine Forest." Forests 13, no. 2 (2022): 225. http://dx.doi.org/10.3390/f13020225.

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This paper reports statistical relationships between measured airflow, air pressure fluctuations, and the wind-induced motion of planted Scots pine trees (Pinus sylvestris L.). The results presented illustrate the potential of low-cost, ground-based air pressure measurements for monitoring wind-induced tree response. It is suggested that air pressure fluctuations can be used as surrogate information for above-canopy airflow, often used to estimate wind loads on forest trees. We demonstrate that air pressure fluctuations can be measured representatively at the forest floor and correlate very we
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Yu, Jinghe, and Patricia Davies. "Improvements to a Method to Simulate Non-Stationary Wind Noise in Vehicles." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 266, no. 2 (2023): 847–57. http://dx.doi.org/10.3397/nc_2023_01_1122.

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As the vehicle and wind speeds and directions change, the unsteady flow creates non-stationary wind noise. To investigate people's perceptions of non-stationary wind noise, a method to simulate the non-stationary wind noise is needed. Previously, a method was developed that used stationary recordings taken at several speeds and directions to create a set of sound pressure level predictions in each one-third octave band that are a function of wind speed and direction. These functions are used to create time-varying filters based on provided wind profiles. A reference wind noise measurement is t
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Zhu, Yuhao, Xu Zhou, Yong Chen, et al. "Comparison of Aerodynamic Effects on the Commonwealth Advisory Aeronautical Research Council (CAARC) Tall Building Model Tested in Two Wind Tunnel Laboratories." Applied Sciences 15, no. 2 (2025): 811. https://doi.org/10.3390/app15020811.

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Wind tunnel test results can be influenced by various factors such as the blockage ratio and scaling ratio. These factors may introduce errors in the experimental outcomes, impacting the accuracy and reliability of the data obtained. This study quantitatively assesses consistency and identifies uncertainty sources to enhance result uniformity across various wind tunnel laboratories. This study conducted a systematic comparison between different wind tunnels in terms of rigid model pressure measurement wind tunnel experiments on the same Commonwealth Advisory Aeronautical Research Council (CAAR
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Liu, Jun, Yuan Quan Yang, Yan Lei Sun, and Bin He. "Simulation Study on the Wind Pressure of Village Flat Roof with Parapet Based on Different Wind Angles." Applied Mechanics and Materials 638-640 (September 2014): 228–32. http://dx.doi.org/10.4028/www.scientific.net/amm.638-640.228.

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The main research methods to predict and research wind loads on buildings at home and abroad include wind tunnel tests, field measurement and numerical simulation. However, the wind tunnel tests and field measurement require big funds, long cycle and complicated measurement. Moreover, numerical simulation technology is quite mature. In this paper, based on fluid dynamics software CFD and criteria Reynolds k-ε turbulence model, wind field of the village flat roof with parapet is studied using the numerical simulation technology. Furthermore, the wind pressure data in different wind angles are p
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DRAKE, STEPHEN A., HENDRIK HUWALD, MARC B. PARLANGE, JOHN S. SELKER, ANNE W. NOLIN, and CHAD W. HIGGINS. "Attenuation of wind-induced pressure perturbations in alpine snow." Journal of Glaciology 62, no. 234 (2016): 674–83. http://dx.doi.org/10.1017/jog.2016.53.

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ABSTRACTWindpumping has been identified as a process that could potentially enhance sublimation of surface snow at high forcing frequency and spawn air movement deeper in firn at lower frequencies. We performed an experiment to examine the relationship between high-frequency wind and pressure measurements within the top meter of an alpine snowpack and compared experimental results with two theoretical predictions. We find that both theoretical predictions underestimate high-frequency perturbation pressure attenuation with depth in the near-surface snowpack and the discrepancy between theory an
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Franek, Michal, Lenka Konecna, Oľga Hubová, and Juraj Žilinský. "Experimental Pressure Measurement on Elliptic Cylinder." Applied Mechanics and Materials 820 (January 2016): 332–37. http://dx.doi.org/10.4028/www.scientific.net/amm.820.332.

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This paper deals with pressure measurement on the surface of the elliptic cylinder. Aerodynamic properties are not same for different shape of the building. Therefore it is important complex experimental measurement for complicated shape. Aim of the article is to understanding the wind loads on building for various arrangements. Results are external pressure coefficients of elliptic model for various rotations. Conclusion of the experiment is to find optimal and critical wind direction for isolated building. This research will be background for future work of interference effect.
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Hou, Tianhao, Hongyan Xing, Wei Gu, Xinyi Liang, Haoqi Li, and Huaizhou Zhang. "Wind Pressure Orthogonal Decomposition Anemometer: A Wind Measurement Device for Multi-Rotor UAVs." Drones 7, no. 6 (2023): 366. http://dx.doi.org/10.3390/drones7060366.

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Wind speed and direction are critical meteorological elements. Multi-rotor unmanned aerial vehicles UAVs are widely used as a premium payload platform in meteorological monitoring. The meteorological UAV is able to improve the spatial and temporal resolution of the elements collected. However, during wind measurement missions, the installed anemometers are susceptible to interference caused by rotor turbulence. This paper puts forward a wind pressure orthogonal decomposition (WPOD) strategy to overcome this limitation in three ways: the location of the sensors, a new wind measurement method, a
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Zhu, Guangxia, Xin Liu, Lulu Liu, and Shengli Li. "Effect of Natural Wind on the Transiting Test for Measuring the Aerodynamic Coefficients of Structures." Symmetry 13, no. 8 (2021): 1493. http://dx.doi.org/10.3390/sym13081493.

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The aerodynamic coefficients transiting test is a new method for measuring the structural aerodynamic coefficients using the wind generated by a moving vehicle. However, the effect and correction of natural wind on the transiting test has not been studied. Hence, in this study, the investigation of the aerodynamic force and pressure measurements on a special triangular prism model is simulated through the transiting test under different natural wind conditions for 30° and 90° angles of wind incidence. Force and pressure measurement results in the transiting test are used to describe and explai
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Bai, Wen Lei, Byun Gik Chang, Gerald Chen, Ken Starcher, David Carr, and Roy Issa. "Small Wind Turbine Power Performance Testing with Uncertainty Analysis." Advanced Materials Research 875-877 (February 2014): 1944–48. http://dx.doi.org/10.4028/www.scientific.net/amr.875-877.1944.

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Wind turbine power performance testing consists of power, temperature, air pressure and wind speed measurements collected for this study during which measuring uncertainties are involved. Due to the measurement uncertainties, the results of power performance testing are affected; therefore, it is necessary to consider the measurement uncertainties for evaluating the accuracy of turbine testing. For this purpose of this study, uncertainty analysis for one 5kW wind turbine power performance testing was conducted. The results of uncertainty analysis indicated that the uncertainty negatively affec
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Dissertations / Theses on the topic "Wind-pressure Measurement"

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Oram, C. E. "Aerodynamic surface pressure measurement in atmosphere and wind tunnel on a vertical axis wind turbine blade using pressure transducers." Thesis, Cranfield University, 1989. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.375937.

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Bysice, Jason. "In-Situ Measurement of Wind Loads for Roof Edge Metal Configurations." Thesis, Université d'Ottawa / University of Ottawa, 2015. http://hdl.handle.net/10393/33002.

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The role of a roof on any building is to separate the interior environment of the building from the exterior environment, thereby making it a crucial component of the building design. Metal roof edges are the first line of defense against wind-induced loads on the roof system; however, data on the nature of these loads acting on the roof edge system is scarce. Previous studies with field measurements of wind pressure acting on the roof edge reported that metal flashings experienced negative pressure. These findings suggest that current building codes in North America (i.e. NBCC and ASCE codes)
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Samad-Suhaeb, Mujahid. "Aerodynamics of battle damaged finite aspect ratio wings." Thesis, Loughborough University, 2005. https://dspace.lboro.ac.uk/2134/10736.

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When an aircraft is aerodynamically or structurally damaged in battle, it may not able to complete the mission and the damage may cause its loss. The subject of aircraft battle survivability is one of critical concern to many disciplines, whether military or civil. This thesis considered and focused on Computational Fluid Dynamics [CFD] predictions and experimental investigations into the effects of simulated battle damage on the low-speed aerodynamics of a fmite aspect ratio wing. Results showed that in two-dimensional [2d] and three-dimensional [3D] CFD simulations, Fluent's® models work rea
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Campbell, Shawn. "Full-scale measurements of wind-induced building motion /." View abstract or full-text, 2005. http://library.ust.hk/cgi/db/thesis.pl?CIVL%202005%20CAMPBE.

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Aouachria, Zéroual. "L'Eolienne Savonius : comportements mécanique et aérodynamique." Aix-Marseille 1, 1987. http://www.theses.fr/1987AIX11062.

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Methode experimentale de mesure des pressions parietales d'un rotor, a axe vertical, de type savonius en rotation. Les resultats obtenus ont ete utilises dans un modele de calcul afin de determiner les parametres mecaniques c::(m)et c::(p) de la machine. Determination des coefficients de trainee et de portance ainsi que du comportement vibratoire du rotor sous l'effet des forces aerodynamiques. Correlation du champ des pressions d'aube avec le systeme des emissions tourbillonnaires engendrees par l'eolienne en rotation. Etude de dispositifs de suspension de type "pilotis" destines a isoler, en
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Beaudet, Laurent. "Étude expérimentale et numérique du décrochage dynamique sur une éolienne à axe vertical de forte solidité." Thesis, Poitiers, 2014. http://www.theses.fr/2014POIT2271/document.

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L'éolienne Darrieus connaît un intérêt accru ces dernières années parce qu'elle représente une solution alternative potentielle de production d'électricité dans les milieux urbains. En particulier,une éolienne de forte solidité peut être choisie car certaines de ses propriétés peuvent être avantageuses pour son implantation proche de zones habitées. A l'inverse, certaines difficultés aérodynamiques émergent. Ce type d'éolienne fonctionne à de faibles vitesses réduites pour lesquelles le décrochage dynamique a un rôle très significatif. L'objectif de ce travail de thèse consiste à compléter la
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Lyu, Zhipeng. "Aerodynamic Wind Tunnel in Passenger Car Application." Thesis, KTH, Mekanik, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-203971.

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The thesis aims to provide an evaluation on the Volvo 1/5th scaled wind tunnel regarding its potentials and capabilities in aerodynamic study. The flow quality in the test section was evaluated. The experiments were performed included measurements of airspeed stability, tunnel-wall boundary layer profile and horizontal buoyancy. A numerical model was developed to predict the boundary layer thickness on the test floor. Repeatability tests were also conducted to establish the appropriate operating regime.A correlation study between the 1/5th scaled wind tunnel (MWT) and full scale wind tunnel (P
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Villafañe, Roca Laura. "Experimental Aerothermal Performance of Turbofan Bypass Flow Heat Exchangers." Doctoral thesis, Universitat Politècnica de València, 2014. http://hdl.handle.net/10251/34774.

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The path to future aero-engines with more efficient engine architectures requires advanced thermal management technologies to handle the demand of refrigeration and lubrication. Oil systems, holding a double function as lubricant and coolant circuits, require supplemental cooling sources to the conventional fuel based cooling systems as the current oil thermal capacity becomes saturated with future engine developments. The present research focuses on air/oil coolers, which geometrical characteristics and location are designed to minimize aerodynamic effects while maximizing the the
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Wang, Chien-Yu, and 王健宇. "Image Processing and Temperature Correction of Pressure-Sensitive Paint for Airofoil Surface Pressure Measurement in Low Speed Wind Tunnel." Thesis, 2019. http://ndltd.ncl.edu.tw/handle/9n7ca7.

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Chen, Szu-Han, and 陳思翰. "Non-Contact Measurement of the Displacement of Flexible Structure and the Back Calculation of the Surface Wind Pressure." Thesis, 2013. http://ndltd.ncl.edu.tw/handle/70031851780337928520.

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碩士<br>國立中央大學<br>土木工程學系<br>101<br>Due to the construction technology development in recent years, high-rise buildings use light weight and high strength materials which causes the structure to be particularly sensitive to the wind-induced vibration effects. Therefore, it is necessary to often conduct wind tunnel experiments to evaluate the wind effect on the design of high-rise building. In this thesis, the dynamic deflection responses of a flexible structure under wind actions in two different flow conditions of wind tunnel experiment were measured through a non-contact imaging analysis. The d
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Books on the topic "Wind-pressure Measurement"

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1961-, Streluk Angella, ed. Wind and air pressure. Heinemann Library, 2008.

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E, Simley, Pao L. Y, and National Renewable Energy Laboratory (U.S.), eds. LIDAR wind speed measurement analysis and feed-forward blade pitch control for load mitigation in wind turbines: January 2010 - January 2011. National Renewable Energy Laboratory, 2011.

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- and NASA Glenn Research Center, eds. Pressure probe designs for dynamic pressure measurements in a supersonic flow field. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Center, Langley Research, ed. Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels. National Aeronautics and Space Administration, Langley Research Center, 1995.

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K, Puram Chith, Upchurch Billy T, and United States. National Aeronautics and Space Administration., eds. Optimization of measurements with pressure sensitive paints. NASA, 1995.

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L, Schultz Larry, and John F. Kennedy Space Center., eds. Comparison of analytical methods for calculation of wind loads. National Aeronautics and Space Administration, John F. Kennedy Space Center, 1989.

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Moshasrov, V. Luminescent pressure sensors in aerodynamic experiments. CWA 22 Corporation, 1998.

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Smith, Stewart Ellis. An instrument for measuring turbulence during wind erosion. Division of Environmental Science, Murdoch University, 1994.

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A, Rivera José, and Langley Research Center, eds. Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel. National Aeronautics and Space Administration, Langley Research Center, 2001.

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B, Gloss Blair, and United States. National Aeronautics and Space Administration., eds. Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel. National Aeronautics and Space Administration, Scientific and Technical Infomraton Branch, 1986.

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Book chapters on the topic "Wind-pressure Measurement"

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Gu, X. J., J. Coll, D. Lye, F. A. Ellis, V. D. Nguyen, and J. Bureau. "An Optical Pressure Measurement System for Wind Tunnel Testing." In Applications of Photonic Technology. Springer US, 1995. http://dx.doi.org/10.1007/978-1-4757-9247-8_51.

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Zhu, Weijun, and Dichen Li. "Additive Manufacturing of Wind Tunnel Test Models for Pressure Measurement." 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_7.

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Azzopardi, Joel. "AI and Machine Learning to extend Meteo-Marine Station Observations into the Future." In Monitoring of Mediterranean Coastal Areas: Problems and Measurement Techniques. Firenze University Press, 2024. https://doi.org/10.36253/979-12-215-0556-6.73.

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The real-time availability of data from coastal meteo-marine stations is crucial for various stakeholders, including port authorities, government agencies, researchers, and the general public. While observation data is fundamental, short-term forecasts can significantly enhance planning and decision-making processes. This study explores the application of Machine Learning (ML) techniques to predict hourly values of air temperature, wind speed, atmospheric pressure, and humidity for the next 24 hours. We evaluate three ML models: Long Short-Term Memory Network (LSTM), Random Forest (RF), and Mu
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Kirmse, C., B. Sammler, and H. E. Fiedler. "Unsteady Measurement of Static Pressure, Velocity and Temperature in the Vicinity of the Nozzle in a Vacuum—Wind—Tunnel." In Fluid Mechanics and Its Applications. Springer Netherlands, 1997. http://dx.doi.org/10.1007/978-94-011-5474-1_33.

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Kikumoto, Hideki, Yichen Wang, Bingchao Zhang, and Hongyuan Jia. "Enhanced Wind Velocity and Pressure Measurement Around Buildings Using Physics-Informed Neural Networks: A Case Study with a Two-Dimensional Urban Street Canyon." In Lecture Notes in Civil Engineering. Springer Nature Singapore, 2024. https://doi.org/10.1007/978-981-97-8309-0_53.

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Bolgar, Istvan, Sven Scharnowski, and Christian J. Kähler. "Effects of a Launcher’s External Flow on a Dual-Bell Nozzle Flow." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_7.

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Abstract Previous research on Dual-Bell nozzle flow always neglected the influence of the outer flow on the nozzle flow and its transition from sea level to altitude mode. Therefore, experimental measurements on a Dual-Bell nozzle with trans- and supersonic external flows about a launcher-like forebody were carried out in the Trisonic Wind Tunnel Munich with particle image velocimetry, static pressure measurements and the schlieren technique. A strongly correlated interaction exists between a transonic external flow with the nozzle flow in its sea level mode. At supersonic external flow condit
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Cheli, F., L. Mariano, D. Rocchi, P. Schito, and G. Tomasini. "Evaluation of the Cross Wind Velocity Through Pressure Measurements on Train Surface." In The Aerodynamics of Heavy Vehicles III. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-20122-1_9.

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Yamada, Y., T. Miyazaki, M. Nakagawa, S. Tsuda, and H. Sakaue. "Global Pressure- and Temperature-Measurements in 1.27-m JAXA Hypersonic Wind Tunnel." In 29th International Symposium on Shock Waves 1. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-16835-7_86.

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Corsi, Cosimo, Bei Wang, Julien Weiss, and Ha Duong Ngo. "Development of a PVDF Piezo-Film Sensor for Unsteady Wall-Pressure Measurements in SBLIs." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-86605-0_4.

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Abstract An innovative, flexible wall-pressure sensor array for unsteady flow conditions has been developed and evaluated in a turbulent shockwave-boundary layer interaction (SBLI) setup at Mach 2. Compared to the previous version, the new sensor’s flexibility makes it easier to fit on different surfaces, while offering enhanced durability and improved sensitivity. The array comprises 18 circular sensors, each with a diameter of $$3\,{\text {mm}}$$ 3 mm , fabricated using screen printing techniques from a thin piezoelectric PVDF film (thickness: $$110\,\upmu {\text {m}}$$ 110 μ m ). Remarkably
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Joseph, Arun, Pawel Flaszynski, Michal Piotrowicz, Piotr Doerffer, and Marcin Kurowski. "Reynolds Number Effects on Shock Wave Boundary Layer Interaction in Highly Loaded Compressor Stator." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-86605-0_13.

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Abstract When an aircraft engine operates at a transonic regime, the Shock Wave Boundary Layer Interaction (SBLI) plays a significant role in aerodynamic performance and its effects are detrimental while operating at low Reynolds conditions. To investigate SBLI effects numerically and experimentally, a linear cascade 3-profile test section has been designed for the IMP-PAN transonic blow-down wind tunnel facility. A novel technique of inlet valves with perforated plates setup has been installed upstream of the test section to reduce the Reynolds number in the test section. Three different Reyn
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Conference papers on the topic "Wind-pressure Measurement"

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Gardner, A. D., and K. Richter. "Boundary Layer Transition Determination for Periodic and Static Flows using Phase-Averaged Pressure Data." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10091.

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A method of boundary layer transition measurement is presented for wind tunnel models instrumented with surface pressure taps. The measurement relies on taking a number of theoretically identical measurements at different times and then analysing the standard deviation of the pressures. Due to the slight unsteady movement of the transition position, a peak in the standard deviation of pressure σCPpeak is found at the transition position, and this is correlated with measurements of the transition position with an infrared camera and hot film anemometers. In contrast to microphone measurements,
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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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Gregorio, Fabrizio. "Heavy Class Helicopter Fuselage Model Performance Improvement using Vortex Generators." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0074-2018-12695.

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Wind-tunnel tests of a heavy-class helicopter model were carried out to evaluate the effectiveness of passive flow control system in alleviating the fuselage parasite drag. An array of counter rotating vortex generators was selected to reduce/remove the flow separation occurring on the rear loading ramp responsible of the high pressure drag. Different technical solution for the VGs design and location were selected with respect to previous work. The basic fuselage geometrically scaled 1:7 of a heavy class helicopter was investigated with and without passive flow control system. The comprehensi
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Wang, Xing, Anand Saxena, and Inderjit Chopra. "Measurement and Validation of a Mach-Scale Rotor Performance and Loads at High Advance Ratios." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11436.

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Reducing the rotor tip speed by slowing down the rotor in forward flight is a viable means of extending the cruise speed of a compound helicopter. However, in a high advance ratio flight regime, many aerodynamic phenomena remain unclear, including the thrust reversal and the dynamic stall that occurs in the reverse flow region of the retreating blade. In order to investigate the performance and vibratory loads characteristics of a high advance ratio rotor, wind tunnel tests were conducted with a Mach-scale 4-blade articulated rotor at 900 RPM, up to advance ratio 1.15. Hub loads, control angle
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"Measurement of wind pressure coefficients of single-span greenhouses using wind tunnel test." In 2015 ASABE International Meeting. American Society of Agricultural and Biological Engineers, 2015. http://dx.doi.org/10.13031/aim.20152190521.

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Vardaki, Eleni, Neil Stokes, Sergey Fonov, and Jim Crafton. "Pressure Sensitive Paint Measurements at the ARA Transonic Wind Tunnel." In 27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-4796.

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Kammeyer, Mark, and Robert Wozniak. "An Uncertainty Analysis for Low-Speed Wind Tunnel Pressure Measurements." In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-2196.

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Asai, Keisuke, Yutaka Amao, Yoshimi Iijima, Ichiro Okura, and Hiroyuki Nishide. "Novel pressure-sensitive paint for cryogenic and unsteady wind tunnel testing." In 21st Aerodynamic Measurement Technology and Ground Testing Conference. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-2527.

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Buck, Gregory. "Simultaneous global pressure and temperature measurement technique for hypersonic wind tunnels." In 21st Aerodynamic Measurement Technology and Ground Testing Conference. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-2649.

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Kurita, Mitsuru, Kazuyuki Nakakita, Kazunori Mitsuo, and Shigeya Watanabe. "Data Processing of Pressure-Sensitive Paint for Industrial Wind Tunnel Testing." In 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference. American Institute of Aeronautics and Astronautics, 2004. http://dx.doi.org/10.2514/6.2004-2189.

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Reports on the topic "Wind-pressure Measurement"

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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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WIND RESISTANCE PERFORMANCE AND REINFORCEMENT MEASURES OF STANDING SEAM METAL ROOFS BASED ON WIND TUNNEL TESTS. The Hong Kong Institute of Steel Construction, 2025. https://doi.org/10.18057/ijasc.2025.21.1.1.

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As an important building envelope structure, metal roofs have been widely used in various large-scale buildings because of their unique advantages such as beautiful shape, lightweight nature, flexibility, and exceptional strength. However, there are still some gaps in the existing research on the wind resistance performance of metal roof systems, which poses a serious threat to life and property. To address this gap, this paper conducted wind tunnel tests of long-span standing seam metal roofs. The basic wind pressure of 0.95 kN/m2, which is once every 100 years. The wind-induced response of t
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STABILITY PERFORMANCE AND WIND TUNNEL TEST OF STEEL HYPERBOLIC COOLING TOWER CONSIDERING SKINNED EFFECT. The Hong Kong Institute of Steel Construction, 2023. http://dx.doi.org/10.18057/ijasc.2023.19.3.10.

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With the development of industry, cooling towers play a very important role in thermal power generation, and steel cooling towers are being used more widely. The surface of cooling towers is covered with profiled panels, and the skinned effect on the mechanical performance and stability of the structure should be considered. At present, most studies on steel cooling towers have not considered the skinned effect. In steel cooling towers, the skin panels are usually connected to members by self-tapping screws., the shearing test of self-tapping screw connection is carried out considering differe
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