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Derivation of the Equations of Motion of a Symmetrical Wing-Tip-Coupled Airplane Configuration With Rotational Freedom at the Junctures
Author:
Schy, Albert A.
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51G12
Link:
https://digital.library.unt.edu/ark:/67531/metadc59003/
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