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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