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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