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An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence
Author:
Axelson, John A.
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A7J13
Link:
https://digital.library.unt.edu/ark:/67531/metadc58187/
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