Cover Image

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
Description
Item Description:"July 2017."
"Prepared for the 9th AIAA Atmospheric and Space Environments Conference sponsored by AIAA, Denver, Colorado, June 5-9, 2017."
"AIAA-2017-4372."
Physical Description:1 online resource (39 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 38-39).