Preliminary Investigation of the Low-Amplitude Damping in Pitch of Tailless Delta- and Swept-Wing Configurations at Mach Numbers From 0.7 to 1.35

Author: D'Aiutolo, Charles T.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L52G09
Link: https://digital.library.unt.edu/ark:/67531/metadc59421/

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