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49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
In this paper, the design and analysis of a distributed turboelectric propulsion system embedded within a split-wing is discussed. The potential for performance and efficiency improvements are significant with such a design. A propulsion system of this style however comes with many tribulations including difficult integration into the wing and strong coupling between the propulsion system and wing aerodynamics. Inlet analysis yielded a union between pressure recovery and inboard wingdoi:10.2514/6.2011-224 fatcat:si2pw7g5nfasxm2nhngnfofcxe