Cover Image

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
Description
Item Description:"July 2019."
"AIAA-2018-3492."
"Prepared for the Aviation Forum sponsored by the American Institute of Aeronautics and Astronautics, Atlanta, Georgia, June 25-29, 2018."
Physical Description:1 online resource (34 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 33-34).