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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