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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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