Independent effects of Reynolds number and Mach number on aerodynamics of an iced swept wing /

Bibliographic Details

Main Author:	Broeren, Andy P. (Author)
Corporate Author:	American Institute of Aeronautics and Astronautics
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2019.
Series:	NASA technical memorandum ; 2019-220012.
Subjects:	Aircraft icing. Airfoils. Computerized simulation. Data bases. Degradation.
Online Access:	https://purl.fdlp.gov/GPO/gpo123987