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Adjoint-based optimisation of rocket engine turbine blades
Axial turbine stages for gas generator cycle type rocket engines typically employ highly-loaded supersonic stator vanes. Consequently, …
B S Sanghera, Nitish Anand, L Souverein, L Penin, M Pini
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Adjoint-Based Aeroelastic Design Optimization Using a Harmonic Balance Method
Turbomachinery blades characterized by highly-loaded, slender profiles and operating under unsteady flow may suffer from aeroelastic …
Nitish Anand, A Rubino, M Pini, P Colonna
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Assessment of FFD and CAD-based shape parametrization methods for adjoint-based turbomachinery shape optimization.
In automated design of turbomachinery, the method used to parametrize the blade shapes is key to ensure robustness and design …
Nitish Anand, S Vitale, M Pini, P Colonna
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