skip to content
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/
< New search