Experimental Research on Noise Reduction for Continuous Transonic Wind Tunnel Loop
Xibei Gongye Daxue Xuebao, 2020 The noise level of wind tunnel test section is respected as one of the most important performance specifications to represent the flow field quality, especially for large scale wind tunnel. According to the acoustic experimental research conducted in the
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Application of Advanced CFD Tools for High Reynolds Number Testing. [PDF]
, 2008 Numerical simulations of the DLR F11 high lift half model in landing configuration in the test section of the ETW wind tunnel have been carried out with the unstructured CFD code DLR TAU.
Wichmann, Georg +3 more
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Lift Interference in Wind Tunnels with Perforated and Solid Walls [PDF]
INCAS Bulletin, 2021 In order to obtain accurate results in wind tunnel testing it is necessary to determine the effect of interaction between the flow around the model and the test section walls.
Mihaela MANEA, Adrian BURGHIU
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Etude numérique et expérimentale de l'écoulement autour d'un rotor éolien [PDF]
, 2013 An improved model of an actuator surface is proposed, representing the flow around a wind turbine. This model was developed in conjunction with a Navier-Stokes solver using a blade element method for the calculation of power and wake development.
MEMON, Asif +2 more
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Testing of calibration models in order to certify the overall reliability of the trisonic blowdown wind tunnel of VTI [PDF]
FME Transactions, 2010 It is strongly recommended that wind tunnel calibrations become a regular part of the operational cycle for any wind tunnel. They facilitate tunnel-totunnel data comparisons. Standard calibration model, representing a generic winged missile configuration,
Damljanović Dijana, Rašuo Boško
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Contemporary frame of measurement and assessment of wind-tunnel flow quality in a low-speed facility [PDF]
FME Transactions, 2018 The requirements for the accuracy of measurements in a wind tunnel test become more and more severe while the complexity of the test increases. In an environment of reduced time available for wind tunnel test and increasing test costs, it is important ...
Ocokoljić Goran +3 more
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Wind tunnel test study on the influence of slat end size changes in transport aircraft
Hangkong gongcheng jinzhanFor conventional layout civil transport aircraft in a low-speed and high lift configuration, the premature of the stall angle of attack causes the aircraft's approach speed to be too high.
YAN Wei +7 more
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A New Method for Adjusting Setting Angle of Rotor Blade for Axial Fan in Wind Tunnel
Xibei Gongye Daxue Xuebao, 2019 Combining the fan aerodynamic efficiency with the wind tunnel pressure loss coefficient, a new equation which points out the inherent relationship of the fan blade setting angle, fan rotating speed and gas flow rate in wind tunnel circuit is derived ...
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Aerospace, 2021 This study conducted wind tunnel tests with consecutive deflection angle changes on a three-dimensional (3D) wing with a control surface to procure aerodynamic data by sweeping the deflection angle. Configuration changes of a wind tunnel test model, such
Ken Wakimoto +3 more
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The Wind-tunnel Test and Unsteady CFD of an Ornithopter Formation [PDF]
, 2017 According to Lissaman and Shollenberger’s article published in Science in 1970, birds fly in formation to reduce the overall energy expenditure for flight. Thus, this work adopted the same principle of flight formation to ornithopters to save energy. Two
Yang, Lung-Jieh
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