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Inside NASA's X-57 Configuration - More than Just Electrifying an AirplaneThe 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.
Document ID
20200006801
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Jeff Viken
(Langley Research Center Hampton, United States)
Date Acquired
May 13, 2020
Subject Category
Aerodynamics
Report/Patent Number
Report Number: NF1676L-30697
NF1676L-30697
Meeting Information
Meeting: EAA AirVenture
Location: Oshkosh, WI
Country: US
Start Date: July 30, 2004
Sponsors: Experimental Aircraft Association
Funding Number(s)
WBS: 107210.02.06.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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