Turboelectric Distributed Propulsion in a Hybrid Wing Body Aircraft
Citations
818 citations
Additional excerpts
...4 MVA each) to produce electricity [55]....
[...]
317 citations
Cites background or methods from "Turboelectric Distributed Propulsio..."
...Aerodynamics FLOPS/drag polar; BLI benefit based on flatplate momentum thickness Design using vortex lattice/boundary layer codes; some CFD for analysis [51, 85, 158] CFD results from similar configuration, with increment for BLI [56] Drag polar L/D correction methods from Torenbeek [16]...
[...]
...The N3-X relies on very advanced technology and claims -70% fuel burn reduction versus the 777-200 benchmark; the portion attributable to electric propulsion is closer to -20%, with much of the remainder a result of airframe and other technologies [56]....
[...]
...Conceptual trade studies so far have favored superconducting architectures for very high-power applications (such as the 300-passenger NASA N3-X) and conventional conductors for megawattclass requirements and below (such as the 150-passenger NASA STARC-ABL) [56, 27]....
[...]
...Subsequently, the concept has been the focus of more detailed analysis and design revision by NASA [56, 29, 58, 59], with refined weights [90] and noise and emissions [91]....
[...]
...[56, 57, 58, 59, 60, 61, 27] Boeing SUGAR Volt 2035 PHE 154 68040 1....
[...]
307 citations
199 citations
140 citations
References
641 citations
491 citations
138 citations
103 citations
97 citations