Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects /

Bibliographic Details

Main Author:	Broeren, Andy P. (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2017.
Series:	NASA technical memorandum ; 2017-219533.
Subjects:	Aerodynamic configurations. Aircraft icing. Computational fluid dynamics. Leading edges. Swept wings.
Online Access:	https://purl.fdlp.gov/GPO/gpo85650