An Analog Study of the Influence of Internal Modifications to a Wing Leading Edge on Its Transient Temperature Rise During Highspeed Flight

Author: Neel, Carr B.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A57K21
Link: https://digital.library.unt.edu/ark:/67531/metadc52906/

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