Aerodynamic drag on deformable and active structures in high Reynolds number conditions by Guttag, Mark A. (Mark Andrew)

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Characterization and mitigation of blade waviness effects on fan performance by Lee, Jinwook,Ph. D.Massachusetts Institute of Technology.

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Methods of Aircraft Charge Control During Flight by Martell, Benjamin C.

“…The system demonstrates comparable results to previous modeling and wind tunnel experiments, which showed an increase in plane potential and a decrease in corona current as wind speed increased. …”
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An Experimental Investigation of Blown-Flap Airfoils by Long, Trevor

“…A quasi 2-dimensional wind tunnel model is used to conduct surveys on both the performance and flow characteristics of propeller blown-flap airfoils. …”
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Design and development of a high-altitude, in-flight-deployable micro-UAV by Tao, Tony S. (Tony Shuo)

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Quantification of the boundary layer ingestion benet for the D8-series aircraft using a pressure rake system by Lieu, Michael K

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Analysis of civil aircraft propulsors with boundary layer ingestion by Hall, David Kenneth

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Development of longitudinal flight simulator by He, Yufan

“…The core simulation engine is built in Simulink and the input are attitudes of the aircraft model in wind tunnel and the forces experienced by the aircraft model in inertial frame of reference. …”
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Investigating Galilean invariance in CFD by Yeo, Beverley Kai Wen

“…When characterizing a body moving in a quiescent flow, like the case of a cruising aircraft, CFD simulations and wind tunnel tests rely on the Galilean invariance principle, which assumes that the moving body can be equivalently modelled by a stationary body with a freestream velocity equal to the motion velocity of the body. …”
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Measurements of a heated low speed channel by Huang, Andy Zi Jie.

“…The low air velocity inside the wind tunnel of the test rig will be controlled and kept constant by a pulse width modulation circuit. …”
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Computational modeling of the aerodynamic characteristics and flight mechanics and control of an unmanned aerial vehicle by Tan, Leon Mark Choon Seng

“…By combining these estimates with wind tunnel data, a comprehensive aerodynamic characteristics model is constructed for augmenting the flight dynamics model of the UAV. …”
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A simplified gas flow meter by Mohamed Nizamudeen Abdul Rahman.

“…The skid set-up comprises of a wind tunnel, filter, slam shut valve and turbine gas meter with the rationale of simulating the actual working conditions of a distribution network regulating station of Town Gas. …”
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Design and development of joined-wing aircraft by Teo, Te Wei

“…Testing was done using both CFD simulations, and wind tunnel testing on actual models, focusing on the lift and drag coefficients. …”
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Actuation and control of wing warping via tendon-sheath mechanism for flexible membrane wing mini-UAV by Lee, Shian

“…Further verifications such as computational fluid dynamic simulations, wind tunnel tests and flight tests were conducted to show the robustness and real world usability of the TSM wing warping controller on the FMW mini-UAV. …”
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Aerodynamics of badminton shuttlecock : Characterization of flow around a conical skirt with gaps, behind a hemispherical dome by Lin, C. S. H., Chua, C. K., Yeo, J. H.

“…Some of the numerical results were validated against wind tunnel experiments. The numerical and experimental results showed good agreement.…”
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Tendon-sheath mechanisms in flexible membrane wing mini-UAVs : control and performance by Tjahjowidodo, Tegoeh, Lee, Shian

“…The proposed approach is validated experimentally in a wind tunnel facility with imitated gusty condition and subsequently tested in a real flight condition. …”
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Studi Eksperimental Perpindahan Kalor dan Penurunan Tekanan Aliran Udara Melintasi Penukar Kalor Kompak Tabung Eliptik Susunan Berseling by , BUDI UTOMO KUKUH WIDODO, , Ir. Samsul Kamal MSc., PhD.

“…Experiments are conducted in the subsonic wind tunnel with air velocity of 1 m/s to 12 m/s under uniform heat fluxes of 3.7 kW/m2, 3.8 kW/m2 and 3.9 kW/m2. …”

Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali by Mohd Ali, Zurriati

“…The experimental works were performed on a scale model and tested in a low speed wind tunnel. Angles of attack, a varied from -10 to 10 degree, as well as canard setting angles, 8. …”
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Longitudinal flight dynamics and stability of blended wing-body unmanned aerial vehicle with canard as control surface / Rizal Effendy Mohd Nasir by Mohd Nasir, Rizal Effendy

“…This study proposes simple scheduled feedback gains to the canard. Wind tunnel experiments, computational simulations and empirical estimations were conducted to characterize its aerodynamics and to come up with its aerodynamic mathematical model for flight dynamics derivatives calculation. …”
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Heat transfer in the core compressor under ice crystal icing conditions by Bucknell, A, McGilvray, M, Gillespie, DRH, Jones, G, Reed, A, Buttsworth, DR

“…The plate was installed in the Altitude Icing Wind Tunnel (AIWT) at the National Research Council of Canada (NRC). …”