High-fidelity aerodynamic and aerostructural optimization of UAV propellers using the adjoint method
AIAA SCITECH 2023 Forum
01.01.2023
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Toward High-Fidelity Aerostructural Optimization Using a Coupled ADjoint Approach
British Library Conference Proceedings | 2008
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