Aero-propulsive Design Optimization of a Turboelectric Boundary Layer Ingestion Propulsion System (AIAA 2018-3976)
Aviation technology, integration and operations (Conference)
01.01.2018
13 pages
Aufsatz (Konferenz)
Englisch
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Thermal cycle analysis of turboelectric distributed propulsion system with boundary layer ingestion
Online Contents | 2013
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