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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