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aerodynamic properties, aerosol-cloud interaction, and transport effects in small and large volumes (e.g., instrumental inlets, atmosphere). Candidates with a strong background in the topical areas of
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, the role involves utilising numerical simulations to investigate the structural and aerodynamic performance of the newly developed wind turbine blade under operational loads. Who we are looking for
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successful candidate will also develop, evaluate and test rotor aerodynamic models and optimal control solutions rotor control. Other projects may be assigned by supervisor depending on skills and technical
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Mathjobs.org | 24 days ago
Biology. Some of the current research projects in Applied Mathematics include laser ablation of biomedical tissues; preventing aerodynamic stall by in-flight ice accretion in the aerospace industry
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and team members to conduct novel research. Key Responsibilities Produce novel computational models of biological systems (e.g. MuJoCo, MJX, Blender, aerodynamic modeling approaches) 30% Apply machine
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Okinawa Institute of Science and Technology | JP Nagar III Phase, Karnataka | India | about 6 hours ago
Biology. Some of the current research projects in Applied Mathematics include laser ablation of biomedical tissues; preventing aerodynamic stall by in-flight ice accretion in the aerospace industry
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research at the aerosol group. Possible areas may span from particle microphysics and mixing state to optical, radiative and aerodynamic properties, aerosol-cloud interaction, and transport effects in
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dynamic response analyses, covering both hydrodynamic and aerodynamic effects, as well as structural integrity analyses. The researcher will collaborate closely with project partners, including
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curriculum, such as the Aerospace Capstone course, AE100. Teaching will include bringing to the class relevant industry or research experience in space or aerodynamic flight. This position will also
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collaborations in the fields of turbine aerodynamics, heat transfer, acoustics and combustion research. The core competence currently lies in the experimental and numerical aerodynamic investigation of single