Cover Image

Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept /

Bibliographic Details
Main Author:	Koning, Witold J. F. (Author)
Format:	Government Document eBook
Language:	English
Published:	Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, November 2018.
Series:	NASA technical memorandum ; 2018-219788.
Subjects:	Angle of attack. Directional stability. Rotary wing aircraft. Computational fluid dynamics. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo114085

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