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Experimental Investigation of the Damping in Roll of Cruciform Triangular Wing-Body Combinations at Mach Numbers From 1.5 to 6.0
Author:
Boissevain, Alfred G.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A54B15a
Link:
https://digital.library.unt.edu/ark:/67531/metadc60115/
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