NASA NTRS · 20200006801
TPSAS-NF1676L-30697-DND
Abstract
The goal of the NASA X-57 Electric Airplane was to utilize the versatility and efficiency of electric propulsion to design a cruise optimized airplane. The wing planform was reduced 42%. A slotted flap and distributed fan system were developed to achieve CL?s in excess of 4.0. Performance objectives, features of the wing and high-lift system, as well as integration considerations will be discussed. CFD performance analysis and details of the integrated structure will be discussed.
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Jeff Viken. TPSAS-NF1676L-30697-DND. https://ntrs.nasa.gov/citations/20200006801
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