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Engineer at the University of Washington Aeronautical Laboratory (UWAL), the research scientist/engineer 1 application assistance and services to wind tunnel customers. The Staff Engineer implements and
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of these models therefore remains a key scientific challenge. In this PhD project, you will develop and apply data-fusion methods that combine physics-based wind farm models with wind tunnel and field data. A
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-processing and validation against wind-tunnel measurements. The resulting tool will subsequently be used to assist design and position optimisation activities. You will be responsible for the following
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to turbulence, shock wave boundary layer interactions in the supersonic and hypersonic regimes. The Aerodynamics laboratories are equipped with state of the art wind tunnels with a large low-speed (low-turbulence
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500 microseconds. In addition to this facility, Dr. DeMauro also directs research in a blowdown wind tunnel that produces flows at Mach 3. Dr. DeMauro’s team of experimentalists comprises six Ph.D
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comprehensive aero lab consisting of a mid-size low speed wind tunnel, a Mach number 4.5 supersonic wind tunnel, and a pressurized water tunnel equipped with state-of-the-art flow diagnostic systems are operated
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of integrating advanced modeling and simulation tools with state-of-the-art wind tunnel testing. The MAC will advance the reliability and complexity of simulations, extend and validate physics models, and develop
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, including the Emerson Cavitation Tunnel, the Princess Royal research vessel, the fully turbulent flow channel, the towing tank and the combined wind, wave and current tank. We are recruiting a new Senior
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Engineering and Aerospace Innovation Complex (MicaPlex), housing several research laboratories (https://erau.edu/research-park/micaplex/labs ), a state-of-the-art subsonic wind tunnel (https
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without building strong evidence that the new method is safe and effective. Wind tunnel experiments of new concepts may be considered, but because of scaling, the involved physical time scales typically