Aerodynamic optimization and drag minimization for the ultra low cost UAV piquero aerodynamic by Liu, Hao

“…The third segment is a full simulation of the Piquero UAV to determine its lift and drag characteristics. …”
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Wind tunnel testing of a ducted-fan unmanned aerial vehicle by Shiah, Zi Yang.

“…The experiments were carried out in a closed-loop wind tunnel with the full-scale MAV at different configurations. Coefficients of lift, drag and pitching moment were first discussed in a simple configuration of varying pitch angle with different wing setups without the propeller motor. …”
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Why travel far to learn? A study of environmental behaviour change experience of residential outdoor environmental education participants by Syed-Abdullah, Sharifah Intan Sharina

Small towing tank for accurate testing of significantly scaled-down ship models by Chung, Hau Kim.

“…Flow simulation was completed on the full ship model using the surface capturing approach with the resistance predicted. …”
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Prediction of Intermittent Fluctuations from Surface Pressure Measurements on a Turbulent Airfoil by Rudy, Samuel H., Sapsis, Themistoklis P.

“…Methods include direct prediction from historical pressure measurements, flow reconstruction followed by forward integration using a full order solver, and data-driven dynamic models in various low dimensional quantities. …”
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Dwarf kingfisher-inspired bionic flapping wing and its aerodynamic performance at lowest flight speed by Mohd Firdaus Bin Abas, Singh, Balbir, Kamarul Arifin Ahmad, Ng, Eddie Yin Kwee, Khan, Tabrej, Sebaey, Tamer A.

“…The history of vertical force and the flow patterns around the wing is captured in a full cycle with asymmetric lift development in a single stroke cycle. …”
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An experimental and simulation study of chip transportation behaviour in gundrilling by Tnay, Guan Leong

“…The experiments were conducted in vertical square tube filled with the water-glycerine solutions which have properties similar to the coolant properties with concentration of 85 % oil to 5 % oil. …”
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Determination of operating point for a propulsive wing UAV using CFD by Chan, Chee Shuan

“…In addition, contour plots of CFD showed wake filling effect of the cross flow fan. General trends for operating points in CFD agrees with that obtained by wind tunnel testing.…”
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