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Experimental Determination of the Yawing Moment Due to Yawing Contributed by the Wing, Fuselage, and Vertical Tail of a Midwing Airplane Model
Author:
Campbell, John P.
Year:
1943
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-L-387, NACA-ARR-3F28
Link:
https://digital.library.unt.edu/ark:/67531/metadc60937/
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