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Flight-determined static lateral stability and control characteristics of a swept-wing fighter airplane to a Mach number of 1.39
Author:
Matranga, Gene J
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-H57A16
Link:
https://digital.library.unt.edu/ark:/67531/metadc63030/
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