Experimental determination of the damping in roll and aileron rolling effectiveness of three wings having 2 degree, 42 degree and 62 degree sweepback

Author: Bennett, Charles V.
Year: 1947
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1278
Link: https://digital.library.unt.edu/ark:/67531/metadc55191/

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