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Free-flight investigation of the control effectiveness of a differentially deflected horizontal tail at Mach numbers from 0.8 to 1.6
Author:
Mitchell, Jesse L.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56B20
Link:
https://digital.library.unt.edu/ark:/67531/metadc62445/
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