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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