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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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