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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
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Hypersonic Aerodynamics. The successful candidate will play a key role in developing and advancing new measurement systems for the departments Hypersonic blowdown wind tunnel, and conducting cutting-edge
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, post-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
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integrate your mathematical models and computational results with their complementary experimental wind-tunnel and water-flume data. Leveraging your strong background in high-fidelity simulations and
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Delft University of Technology (TU Delft) | Delft, Provincie Zuid-Holland | Netherlands | 21 days ago
with wind tunnel and field data. A particular focus will be on exploiting the extensive experimental data generated within the HKN project, including measurements from wind-tunnel experiments and full
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of Engineering/MoD Research Chair in Hypersonic vehicles. He has led the development of multiple large scale hypersonic wind tunnels, including the Oxford High Density Tunnel and the Oxford T6 Stalker
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simulations, advanced aerodynamic models, and multidisciplinary rotor design and investigation of new concepts in interaction with the industry. The Poul la Cour Wind Tunnel, the Rotating Test Rig and the
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, facilitating Fluid Structure Interaction methods and multidisciplinary rotor design and investigation of new concepts in interaction with the industry. The Poul la Cour Wind Tunnel, the Rotating
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Delft University of Technology (TU Delft) | Delft, Provincie Zuid-Holland | Netherlands | about 2 months ago
-speed (low-turbulence) wind tunnel and high-speed transonic-supersonic tunnels up to hypersonic flows (Mach 11). A low-speed open test section large wind tunnel (Open Jet Facility) erected in 2008 is
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envisaged for wind-tunnel experiments aimed at calibrating aerodynamic models and improving the velocity prediction tools used for trajectory optimization. The expected outcome is both scientific and