Design of a Distributed Propulsion Concept Using an Adjoint-Based Approach and Blade Element Theory to Minimize Power
AIAA AVIATION 2020 FORUM
2020-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA-2019-3681: Adjoint-Based Design of a Distributed Propulsion Concept with a Power Objective
British Library Conference Proceedings | 2019
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