Numerical simulation of the boundary layer development behind a single quarter elliptic-wedge spire by M. A., Fitriady, Nurizzatul Atikha, Rahmat, A. F., Mohammad, S. A., Zaki

“…For decades wind tunnel has been utilized to generate a quasi-atmospheric boundary layer to observe the wake flow around objects submerged within the Atmospheric Boundary Layer. …”
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High Resolution Modelling of Traffic Emissions Using the Large Eddy Simulation Code Fluidity by Huw Woodward, Anna K. Schroeder, Clemence M. A. Le Cornec, Marc E. J. Stettler, Helen ApSimon, Alan Robins, Christopher Pain, Paul F. Linden

“…Fluidity showed an acceptable comparison with the wind tunnel data for velocities and turbulence intensities. …”
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Propeller-induced effects on the aerodynamics of a small unmanned aerial vehicle by Maqsood, Adnan, Huei, Foong Herng, Go, Tiauw Hiong

“…Specifically, the slipstream effects on the aerodynamics of a generic small unmanned air vehicle are studied in the wind tunnel for the shift in the aircraft stall angle of attack. …”
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Experimental aerodynamics of washout twist morphing MAV wing / Muhammad Hakim Mohd Hafiz by Mohd Hafiz, Muhammad Hakim

“…A suitable test rig is also developed for wind tunnel testing. Four TM wing configurations (Membrane, TM1N, TM3N and TM5N) are subjected to wind tunnel procedure. …”
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CFD analysis on propeller at varying propeller disc angle and advance ratio by Leong, Chee Hang, Rosli, Nur Athirah Nadwa, Ab. Wahid, Mastura, Othman, Norazila, Mat, Shabudin, Md. Zain, Mohd. Zarhamdy

“…The purpose of this study is to see the feasibility of using Computational Fluid Dynamic (CFD) analysis over wind tunnel testing for propeller performance measurement. …”
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Design of sail performance rig ... [et al.] / [microfilm] by 255271 Kanagaprakasam Rasaretnam

CFD Analysis of Wind Interference Effects of Three High-rise Buildings by Qiong* Xing, Jiang Qian

“…The numerical results were in good agreement with wind tunnel test results, demonstrating the feasibility of the numerical model. …”
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An Algorithm for Estimation of Wind-Building Interaction in the Early Design Stage by İlker Karadağ, Nuri Serteser

“…Wind-building interaction can be estimated with one of three approaches, or a combination of these: (1) on-site measurements, (2) reduced-scale wind tunnel measurements or (3) numerical simulation based on Computational Fluid Dynamics (CFD). …”
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Fully Mechatronical Design of an HIL System for Floating Devices by Hermes Giberti, Francesco La Mura, Gabriele Resmini, Marco Parmeggiani

“…To make up for the lack of experimental data, usually wind tunnel and ocean basin tests are carried out. This paper presents a fully mechatronical design of an Hardware In the Loop (HIL) system capable of simulating the effects of the sea on a physical scaled model positioned in a wind tunnel. …”
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Modèle d'accrétion de glace sur un objet bidimensionnel fixe appliquable aux pales d'éoliennes by Guy Fortin, Adrian Ilinca, Jean-Louis Laforte

“…The accretion model was validated for dry and wet regimes with ice profiles obtained by Shin and Bond in wind tunnel experiments. The ice profiles numerically predicted are similar to those measured in wind tunnel and the model is able to generate the complex ice profiles observed in experiments, such as horns and grooves. …”
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Design of Control Law of Post Stall Maneuver under Unsteady Aerodynamics Based on Improved Dynamic Inverse Method

“…Firstly, depending on the wind tunnel experimental data of the advanced fighter aircraft model under biaxial coupled large oscillation, an accurate unsteady aerodynamic model is established by using the improved extreme learning machine (ELM) method. …”
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Experimental and Numerical Studies on Improvement of Aerodynamic Performance of a Semi-trailer Truck Model Using the Cabin Spoiler by Stjepan Galamboš, Nenad Poznanović, Nebojša Nikolić, Dragan Ružić, Jovan Dorić

“…The achieved results were confirmed by experimental tests in a wind tunnel.…”
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COMPUTATIONAL ANALYSIS OF LOAD VENTILATION IN BROILER TRANSPORT by Daniel G. Pinheiro, Nítalo A. F. Machado, José A. D. Barbosa Filho, Iran J. O. Da Silva

“…Computational fluid dynamics (CFD) simulations and wind tunnel tests were performed using small scale models. …”
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Drag Reduction of Semi-Trailer Aerodynamic Devices Determined by Two Different Methods by Tomáš Skrúcaný*, Štefánia Semanová, Jozef Gnap, Tomasz Figlus, Jiří Čupera

“…The results were compared with drag coefficient values examined in a wind tunnel test on a scaled truck model done by authors.…”
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Design and analysis of a vertical axis wind turbine by Koh, Jian Hao.

“…The CFD simulations suggested that the P C values could be augmented in a wind tunnel test.…”
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Investigation of pressure drop over textured surfaces by Huang, Huolin

“…In this work, randomized longitudinal riblets produced by sandpapers with different grit sizes were investigated in a close-loop wind tunnel, the experiment was designed to elevate the textured surfaces from the wind tunnel wall at zero pressure gradient. …”
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Development of wind turbine main rotor shaft torque measurement device / Ahmad Safuan Mohd Yusoff by Mohd Yusoff, Ahmad Safuan

“…The experiment will be conducted in the wind tunnel. This device is able to measure torque at speed of wind ranging between 0 to 15m/s in the wind tunnel in our faculty. …”
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Tool for Rapid Transient Transpiration Cooled Re-Entry Simulation - Dataset by Hermann, T, Naved, I, McGilvray, M

“…The code is validated with experimental data of plasma wind tunnel tests and the SHEFEX II flight experiment. …”

The effect of adding diffuser by experimental by Samion, Syahrullail, Musa, Mohamad Nor, Ansorudin, Ruwaida, Mohd. Salleh, Zuan Azhary

“…It is done by determining each of the drag coefficient of the model, by experimental method using Low Speed Wind Tunnel. All the relevant data are collected through the literature reviews from books and journals. …”

Experimental work on unsteady helicopter rotor hub wakes by Ishak, I. S., Mansor, S., Lazim, T. M., Mat, S., Md. Zain, M. Z., Mohd. Nasir, R. E., Mohd. Ali, Z.

“…This research work is intended to investigate the unsteady aerodynamic wake characteristics induced by the helicopter rotor hub that lead to this tail shake phenomenon by executing a wind tunnel campaign. The experiments were carried out in the UTM wind tunnel with a test section of 2m (width) × 1.5m (height) × 5.8m (length) with the maximum wind speed of 80m/s. …”