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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