Free-flight investigation to determine some effects of tail damping and wing-tail interference on the rolling effectiveness of ailerons and a spoiler on a modified-delta wing at Mach numbers from 0.6 to 1.5

Author: English, Roland D
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57C13
Link: https://digital.library.unt.edu/ark:/67531/metadc63303/

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