Low-Speed Roll Effectiveness of a Differentially Deflected Horizontal-Tail Surface on a 42 Degree Swept-Wing Model

Author: Boisseau, Peter C.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56E03
Link: https://digital.library.unt.edu/ark:/67531/metadc53079/

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