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related technical field, where prior research experiences in the analysis of aerodynamic noise, vortex sound, and/or wave scattering are highly valued. The postdoctoral scholar will benefit from
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carries out technology research and development on flight vehicles, flight physics, aerodynamics, thermodynamics and fluidic engineering. The Section is also the focal point for the architecture design
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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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experience on numerical modelling of aerodynamic and/or hydrodynamic loading on structures. The applicants shall demonstrate the following experiences: Teaching at undergraduate and graduate levels
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, aerodynamic, and aeroelastic testing. Develop and apply advanced numerical models (e.g., FEA, CFD) to simulate wind effects on structures. Analyze and interpret experimental and numerical data, and disseminate
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position in active flow control for wingsail performance and operation. The goal is to develop innovative flow control techniques to optimize aerodynamic performance and reduce vibrations in unsteady
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experience on numerical modelling of aerodynamic and/or hydrodynamic loading on structures. The applicants shall demonstrate the following experiences: Teaching at undergraduate and graduate levels
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National Aeronautics and Space Administration (NASA) | Fields Landing, California | United States | 3 months ago
atmospheric entry, modeling of fragmentation during entry, aerothermodynamics of asteroid entry, and the aerodynamics of multi-body flight. Impact hazard research involves the creation of reduced order models
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-hypersonic realm. The postdoctoral scholar will offer multidisciplinary research skills, adapting to the convolution of aerodynamic, aerothermal and materials fields. The researcher will co-ordinate
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digital systems engineering, with particular emphasis on the development of a model-based digital twin of the system design disciplines (i.e. aerodynamics, thermal, trajectory and flight mechanics