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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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