Computational Fluid Dynamics Analysis of Spray Cooling in Australia by Puchanee Larpruenrudee, Doan Khai Do, Nick S. Bennett, Suvash C. Saha, Mohammad Ghalambaz, Mohammad S. Islam

“…Due to the effect of spray cooling inside the wind tunnel, the temperature at the outlet is still lower than the inlet for all cases. …”
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Effect of Flexible Flaps on Lift and Drag of Laminar Profile Flow by Artur Reiswich, Max Finster, Martin Heinrich, Rüdiger Schwarze

“…An NACA0020 profile was mounted on a force balance and placed in a wind tunnel. Elastic flaps were attached in rows at different positions on the upper profile surface. …”
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Measuring cycling kinematics using a low-cost, flashing LED, multi-camera approach by Gilbertson, Matthew (Matthew W.)

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An experimental and theoretical study of the ice accretion process during artificial and natural icing conditions by Kirby, Mark Samuel, Hansman, Robert John

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System identification of aerodynamic derivatives for VTOL UAV by Matiin Muhammad Hanifah Marican

“…The model was constrained to pitch freely while mounted on a rig placed within a wind tunnel test section. A servo motor was used to provide controlled inputs to the elevator, and an Inertial Measurement Unit (IMU) was used to measure the pitch angle and pitch rate. …”
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Experimental investigation of a bi-planar micro air vehicle by Chang, Collin Wei Teck.

“…The Main Aircraft Laboratory low speed, low turbulence closed loop wind tunnel was used to test the full scale bi-planar prototype at various geometric configurations. …”
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Design and analysis of a vertical axis wind turbine by Chue, Wai Yong.

“…In this project, a Delta Blade VAWT was designed and built for wind tunnel testing. Initially, the Delta Blade VAWT with standard delta blades obtained a maximum power coefficient of 0.0138. …”
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Studies of aerodynamics of supersonic generic round shaped bodies by Wanchai, Jiajan

“…For the aerodynamic testing, to validate the superior performance of an optimum geometry obtained using the optimization procedure, the new optimum round and the standard 155 mm M549 body were tested in the large-size, high flow quality supersonic wind tunnel under non-spinning conditions. The wind tunnel test successfully demonstrated the accuracy and effectiveness of the optimization procedure.…”
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Prediction of aerodynamic characteristics of an aircraft model with and without winglet using fuzzy logic technique by Hossain, Altab, Rahman, Mohammed Ataur, Hossen, Jakir, Iqbal, Parvez, M.I., Zahirul

“…Based on the longitudinal aerodynamic characteristics analyzing for the aircraft model tested in low subsonic wind tunnel, the lift coefficient (CL ) and drag coefficient (CD) were investigated respectively. …”
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Assessing landscape dust emission potential using combined ground‐based measurements and remote sensing data by von Holdt, J, Eckardt, F, Baddock, M, Wiggs, G

“…In this study, we used dust emission source points identified in Namibia with Landsat imagery together with field‐based dust emission measurements using a Portable In‐situ Wind Erosion Laboratory wind tunnel to assess the performance of schemes aiming to represent erodibility in global dust cycle modeling. …”

Estimation of Aerodynamic Characteristics of a Light Aircraft by Ishak, Iskandar Shah, Mat, Shabudin, Mat Lazim, Tholudin, Muhammad, Mohd. Khir, Mansor, Shuhaimi, Awang, Mohd Zailani

“…This paper presents the aerodynamic estimation carried out on a three-dimensional aircraft model by conducting wind tunnel tests and Computational Fluid Dynamics (CFD) simulation. …”
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Experimental study on perfomance of wind catcher in tropical climate by Gharakhani, A., Sediadi, E., Roshan, M., Sabzevar, H. B.

“…This paper aims to study how the wind catcher works by the wind-tunnel testing and CFD simulations. The main objective of this research is to discover how a wind catcher works by considering climate situations of a tropical region. …”
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Aerodynamic characteristics of a cranked planform blended wing-body aircraft with 40° sweep angle by Ahmad, A. M., Nasir, R. E. M., Latif, Z. A. A., Kuntjoro, W., Wisnoe, W., Ishak, I. S.

“…The experiment is conducted at UTM-LST Wind Tunnel, AEROLAB, Skudai, Johor with test wind speed of 15 m/s. …”
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Testing and evaluation of flapping wing mechanism by Indra Gunawan

“…Apparatus such as whirling arm test rig and the wind tunnel are used to test and evaluate the flight performance and characteristic of the different wing designs used onto the flapping mechanism.…”
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Wind Loading on Scaled Down Fractal Tree Models of Major Urban Tree Species in Singapore by Woei-Leong Chan, Yong Eng, Zhengwei Ge, Chi Wan Calvin Lim, Like Gobeawan, Hee Joo Poh, Daniel Joseph Wise, Daniel C. Burcham, Daryl Lee, Yongdong Cui, Boo Cheong Khoo

“…It is observed that the velocity profiles and drag of the simulations and the wind tunnel tests are in reasonable agreement. We hence established a clear relationship between the measured bulk drag on the tree models in the wind tunnel, and the local drag coefficients of the discretized elements in the simulations. …”
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Application of Dual Lead Cylindrical Worm in Equipment Renovation by Zhang Leile, Zhang Dewei, Lu Zhihui, Qiao Yongqiang, You Guangfei

“…In the light of renovation requirements of a wind tunnel mechanism,based on the analysis of the equipment characteristics and the characteristic of existing drive mechanism,the existing mechanism is replaced by using the dual lead cylindrical worm. …”
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Heat flux and skin friction on surface of a cone in supersonic flows by T'ng, Alvin Weiheng

“…This is toward the end of preparation for wind tunnel experiments.…”
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Experimental and Simulation Investigation of Performance of Scaled Model for a Rotor of a Savonius Wind Turbine by Kumail Abdulkareem Hadi Al-Gburi, Balasem Abdulameer Jabbar Al-quraishi, Firas Basim Ismail Alnaimi, Ee Sann Tan, Ali Hussein Shamman Al-Safi

“…Hence, to address the challenge of developing a model that resolves these problems, the purpose of this investigation was to determine how well a scaled-down version of a Savonius turbine performed in terms of power output using a wind tunnel. Subsequently, the effect of the blockage ratio produced in the wind tunnel during the chamber test on the scaled model was evaluated. …”
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Overview of the SmartX Wing Technology Integrator by Roeland De Breuker, Tigran Mkhoyan, Nakash Nazeer, Vincent Stuber, Xuerui Wang, Iren Mkhoyan, Roger Groves, Sybrand van der Zwaag, Jurij Sodja

“…The hardware integration platform is chosen to be a wind tunnel model of a low-speed aircraft wing such that it can be tested in a large university-level wind tunnel. …”
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URock 2023a: an open-source GIS-based wind model for complex urban settings by J. Bernard, J. Bernard, J. Bernard, F. Lindberg, S. Oswald

“…Then it is evaluated against wind tunnel measurements and QUIC-URB simulations for four different building layouts plus one case with an isolated tree. …”
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