Ice-accretion test results for three large-scale swept-wing models in the NASA Icing Research Tunnel /

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, September 2016.
Series:	NASA technical memorandum ; 2016-219137.
Subjects:	Aerodynamic characteristics. Aircraft icing. Computational fluid dynamics. Computerized simulation. Three dimensional models.
Online Access:	https://purl.fdlp.gov/GPO/gpo77243