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Theoretical lift due to wing incidence of slender wing-body-tail combinations at zero angle of attack
Author:
Sacks, Alvin H
Year:
1956
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3796
Link:
https://digital.library.unt.edu/ark:/67531/metadc56041/
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