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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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