Conceptual Design of Distributed Electrified Boundary Layer Ingesting Propulsors for the CHEETA Aircraft Concept
AIAA Propulsion and Energy 2021 Forum
01.01.2021
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
An aircraft with fuselage aft end tapering portions and boundary layer ingesting propulsors
Europäisches Patentamt | 2018
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