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Effects of Wing Position and Fuselage Size on the Low-Speed Static Rolling Stability Characteristics of a Delta-Wing Model
Author:
Goodman, Alex
Year:
1955
Document Type:
N/A
Series:
NACA Technical Reports
Report Number:
NACA-TR-1224
Link:
https://digital.library.unt.edu/ark:/67531/metadc65697/
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