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

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Bibliographic Details
Main Author: Broeren, Andy P. (Author)
Corporate Author: American Institute of Aeronautics and Astronautics
Format: Government Document Electronic eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2019.
Series:NASA technical memorandum ; 2019-220012.
Subjects:
Online Access:CONNECT