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Theoretical Calculation of the Effect of the Fuselage on the Spanwise Lift Distribution on a Wing
Author:
Zlotnick, Martin
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51J19
Link:
https://digital.library.unt.edu/ark:/67531/metadc58939/
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