Tests of a Horizontal-Tail Model through the Transonic Speed Range by the NACA Wing-Flow Method

Author: Adams, Richard E.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L7C25a
Link: https://digital.library.unt.edu/ark:/67531/metadc63801/

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