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will be extended to three-dimensional roughness configurations, requiring the development of dedicated numerical tools optimized for high-performance computing environments. Results will be
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, turbines rotate at speeds up to 100,000 rpm to deliver propellant to the rocket engine at high flow rates and optimized pressures. At such extreme conditions, mechanical supports like ball bearings alone
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and optimization with a focus on the design of a robust reusable first stage with respect to model hypotheses (emissions, LCA) and uncertainties. Research Objectives: Development of a multidisciplinary
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