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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