Free-Flight-Tunnel Investigation of the Effect of the Fuselage Length and the Aspect Ratio and Size of the Vertical Tail on Lateral Stability and Control

Author: Shortal, Joseph A.
Year: 1943
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-487, NACA-ARR-3D17
Link: https://digital.library.unt.edu/ark:/67531/metadc61026/

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