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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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