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Low-Reynolds Number Aerodynamics of an 8.9 Percent Scale Semispan Swept Wing for Assessment of Icing EffectsThis paper presents the results of an experimental and computational study of low-Reynolds number swept wing aerodynamics. This work has been conducted in preparation for icing effects on a swept wing. A complete abstract will be written for the final paper.
Document ID
20170007300
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Broeren, Andy (NASA Glenn Research Center Cleveland, OH United States)
Woodard, Brian (Illinois Univ. at Urbana-Champaign Urbana, IL, United States)
Diebold, Jeff (Illinois Univ. at Urbana-Champaign Urbana, IL, United States)
Moens, Frederic (Office National d'Etudes et de Recherches Aerospatiales Noe, France)
Date Acquired
August 3, 2017
Publication Date
June 5, 2017
Subject Category
Numerical Analysis
Aerodynamics
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN43099
Meeting Information
Meeting: AIAA Atmospheric and Space Environments Conference 2017
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 081876.02.03.08.02.02
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aerodynamics
Aircraft icing
Scale models

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