Comparison between fiber bragg gratings and conventional pressure sensor in surface pressure analysis of generic transport aircraft by Miskon, Muhammad Izuan

“…The wind tunnel test was conducted at the wind speed, v in the range of 20 m s -1 to 40 m s -1 and the angle of attack, a in the range of 0° to 20°. …”
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Aerodynamic characteristics of compound wing configuration of wing-in-ground effect vehicle by Jamei, Saeed

“…The experiments carried out in Universiti Teknologi Malaysia low speed wind tunnel and the aerodynamic forces and moment were measured with a Multi-Axis Load Cell JR3. …”

Evaluation of a two-sided windcatcher integrated with wing wall (as a new design) and comparison with a conventional windcatcher by Nejat, P., Calautit, J. K., Majid, M. Z. A., Hughes, B. R., Zeynali, I., Jomehzadeh, F.

“…This research used two main investigative steps: experimental scaled wind tunnel testing and Computational Fluid Dynamics (CFD) simulation. …”

Tomography systems and sensor application for sharp-edged delta wing analysis by Bathusha, Mohamed Salman Sikandar, Mat, Shabudin, Izzuddin, Fahmi, Kasim, Khushairi Amri

“…This paper presents the results on wind tunnel testing above non-slender sharp-edged delta wing under pitching motion. …”
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Analysis of Static Stability and Maneuverability of a New Type of Gyroplane by Tomasz Łusiak

“…The measurements were carried out on a specialized wind tunnel test stand equipped with a dedicated aerodynamic weighing system. …”
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Measuring concentration with Voronoï diagrams: the study of possible biases by Romain Monchaux

“…We have recently proposed to use Voronoï diagrams to estimate concentration fields from two-dimensional imaging techniques implemented around wind tunnel experiments. Due to various experimental biases, the relevance of such an analysis becomes questionable. …”
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Aerodynamic characterisation of porous fairings: pressure drop and Laser Doppler Velocimetry measurements by Fabien Méry, Delphine Sebbane

“…Abstract Wind tunnel measurements of pressure drop and steady and unsteady velocity field of a flow through fairing samples are described. 10 samples have been tested in pressure drop among which the velocity fields of 3 samples have been characterized by means of laser Doppler velocimetry. …”
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Aerodynamic measurements of an airfoil with a spoiler by Gu, Weidong.

“…This thesis presents an experimental study carried out on a NACA 0012 airfoil equipped with a rapidly erected spoiler in a low-speed wind-tunnel. Emphasis is placed on the reduction of the adverse lift and moment because not much on this aspect has been reported in the literature.…”
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Experimental investigation of aeroacoustic damping performance of coupled Helmholtz resonator by Koh, You Jia

“…This experiment will look into the performance of the perpendicularly-coupled Helmholtz resonator, investigated with three different configurations under cold flow condition in a wind tunnel with wind speed from 0 m/s to 20 m/s.…”
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Preliminary Stability Estimation And Analysis Of AEROMECH I UAV Using DATCOM Software by Abdullah, Azizul

“…Conventional methods such as wind tunnel test, flight test and Computational Fluid Dynamics (CFD) are used for the estimation and analysis of the stability during aircraft design process. …”
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Design of stick-framed wood roofs under tornado wind loads by Caspar L. D. Bain, Caspar L. D. Bain, Gregory A. Kopp , Gregory A. Kopp , Ayman M. El Ansary 

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Numerical Simulation and Analysis of Droplet Drift Motion under Different Wind Speed Environments of Single-Rotor Plant Protection UAVs by Juan Wang, Xiaoyi Lv, Bohong Wang, Xinguo Lan, Yingbin Yan, Shengde Chen, Yubin Lan

“…This study used a combination of computational fluid dynamics (CFD) and wind tunnel experiments to analyze the droplet deposition drift pattern of the 3WQF120-12 single-rotor plant protection UAV. …”
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Investigating and Analyzing the Potential for Regenerating Excess Energy in a Helicopter UAV by Chindanai Kodchaniphaphong, Jay-tawee Pukrushpan, Chaiwat Klumpol

“…The simulations were validated by comparing the lift force with wind tunnel experimental data, resulting in acceptable deviations. …”
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Performance Evaluation of a Piezoelectric Energy Harvester Based on Flag-Flutter by Hassan Elahi, Marco Eugeni, Federico Fune, Luca Lampani, Franco Mastroddi, Giovanni Paolo Romano, Paolo Gaudenzi

“…The flag is subjected to the axial airflow in the subsonic wind tunnel. The performance evaluation of the harvester and aeroelastic analysis is investigated numerically and experimentally. …”
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An assessment of electric STOL aircraft by Courtin, Christopher B.(Christopher Bryce)

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Design and analysis on small scale fixed-pitch Straight Bladed Vertical Axis Wind Turbine (SB-VAWTs) by Ji, Xiao Na

“…In the area of experimental studies, wind tunnel tests were carried out a small-scale SB-VAWT fitted with three and four blades. …”
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Gas turbine fouling tests: Review, critical analysis, and particle impact behavior map by Suman, A, Casari, N, Fabbri, E, Pinelli, M, Di Mare, L, Montomoli, F

“…Experimental tests have been carried out on (i) a full scale gas turbine unit, (ii) wind tunnel testing or hot gas facilities using stationary cascades, able to reproduce the same conditions of gas turbine nozzle operation and finally, (iii) wind tunnel testing or hot gas facilities using a coupon as the target. …”

Fortran program utilizing panel method on arbitrary lifting airfoil in two-dimensional incompressible flow to obtain Cl, Cd & Cm / Abdul Rahman Abdullah by Abdullah, Abdul Rahman

“…These special shapes did not represent the optimum in airfoil performance, and experimental methods (that is the wind tunnel testing) guided by theory were used to determine the characteristics of arbitrary shaped airfoils. …”
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Attraction and consumption of methyl eugenol by male Bactrocera umbrosa Fabricius (Diptera: Tephritidae) promotes conspecific sexual communication and mating performance by Wee, Suk Ling, Abdul Munir, M. Z., Hee, Alvin Kah Wei

“…Male attraction to ME peaked from 10 to 27 DAE, which corresponded with the flies’ attainment of sexual maturity. In wind-tunnel assays during the dusk courtship period, ME-fed males exhibited earlier calling activity and attracted a significantly higher percentage of virgin females compared with ME-deprived males. …”
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Experimental research on helicopter tail shake phenomenon by Ishak, Iskandar Shah, Mansor, Shuhaimi, Mat Lazim, Tholudin

“…As the induced wake, which consequently causing tail to shake, differs with pitch and yaw angle, the wind tunnel test was performed in a range of -10o to +10o of pitch and yaw angle, respectively. …”
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