Partially Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters
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[1] Douglas P. Wells,et al. Mission Analysis and Aircraft Sizing of a Hybrid-Electric Regional Aircraft , 2016 .
[2] James L. Felder,et al. Conceptual Design of a Single-Aisle Turboelectric Commercial Transport With Fuselage Boundary Layer Ingestion , 2016 .
[3] Cheryl L. Bowman,et al. Sizing Power Components of an Electrically Driven Tail Cone Thruster and a Range Extender , 2016 .
[4] Gerald V. Brown,et al. Turboelectric Aircraft Drive Key Performance Parameters and Functional Requirements , 2015 .
[5] Gerald V. Brown,et al. Weights and Efficiencies of Electric Components of a Turboelectric Aircraft Propulsion System , 2011 .
[6] Francisco M. Capristan,et al. Conceptual Design of the Parallel Electric-Gas Architecture with Synergistic Utilization Scheme (PEGASUS) Concept , 2017 .
[7] Gerald V. Brown,et al. Partially Turboelectric Aircraft Drive Key Performance Parameters , 2017 .