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Summary and Analysis of Horizontal-Tail Contribution to Longitudinal Stability of Swept-Wing Airplanes at Low Speeds
Author:
Neely, Robert H.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55E23A
Link:
https://digital.library.unt.edu/ark:/67531/metadc53109/
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