Cover Image

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
Description
Item Description:"September 2016."
"Prepared for the 8th Atmospheric and Space Environments Conference sponsored by the American Institute of Aeronautics and Astronautics, Washington D.C., June 13-17, 2016."
"AIAA-2016-3733."
Physical Description:1 online resource (34 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 32-34).