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The effect of tip tanks on the rolling characteristics at high subsonic Mach numbers of a wing having an aspect ratio of 3 with quarter-chord line swept back 35 degrees
Author:
Kuhn, Richard E
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L9J19
Link:
https://digital.library.unt.edu/ark:/67531/metadc58416/
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