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Proc. ASME. GT2021, Volume 2D: Turbomachinery — Multidisciplinary Design Approaches, Optimization, and Uncertainty Quantification; Radial Turbomachinery Aerodynamics; Unsteady Flows in Turbomachinery, V02DT36A016, June 7–11, 2021
Paper No: GT2021-59717
... Proceedings of ASME Turbo Expo 2021 Turbomachinery Technical Conference and Exposition GT2021 June 7-11, 2021, Virtual, Online GT2021-59717 STRUCTURALLY CONSTRAINED AERODYNAMIC ADJOINT OPTIMISATION OF HIGHLY LOADED COMPRESSOR BLADES Cleopatra Cuciumita1, Alistair John1, Ning Qin1, Shahrokh...
Proc. ASME. GT2020, Volume 11: Structures and Dynamics: Structural Mechanics, Vibration, and Damping; Supercritical CO2, V011T31A009, September 21–25, 2020
Paper No: GT2020-14790
... performance of three sCO 2 cycles; simple recuperative, recompression and partial-cooling cycles are studied. Multi-objective optimisation was performed and the off-design Pareto fronts were compared for the changes in the power cycle boundary conditions. Annual performance simulation was carried out...
Proc. ASME. GT2002, Volume 3: Turbo Expo 2002, Parts A and B, 915-923, June 3–6, 2002
Paper No: GT2002-30480
... to suppress the creation of vortices in rotor cavities. CFD Modelling Offtake Passages Optimisation Proceedings of ASME Turbo Expo 2002: ASME Turbo Expo: Land, Sea & Air 2002 June 3-6, 2002, Amsterdam, The Netherlands ta G used to suppress the creation of vortices in rotor cavities. Keywords: CFD...
Proc. ASME. GT2006, Volume 6: Turbomachinery, Parts A and B, 1395-1405, May 8–11, 2006
Paper No: GT2006-90771
..., with a further and deeper insight on this specific design problem. Optimisation Turbine Blade Tip Cooling Heat Transfer Genetic Algorithms Expert systems (Neural Net) Proceedings of ASME TurboExpo 2006: 8-11 May 2006, Barcelona, Spain Proceedings of GT2006 1 Copyright © by ASME Daniele Coutandin...