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Static longitudinal and lateral stability and control characteristics of a model of a 35 degree swept-wing airplane at a Mach number of 1.41
Author:
Palazzo, Edward B.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54G08
Link:
https://digital.library.unt.edu/ark:/67531/metadc60780/
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