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Dynamic Longitudinal Stability Characteristics of a Swept-Wing Fighter-Type Airplane at Mach Numbers Between 0.36 and 1.45
Author:
Wolowicz, Chester H.
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-H56H03
Link:
https://digital.library.unt.edu/ark:/67531/metadc64234/
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