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Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with an aspect ratio 4 triangular wing and an all-movable horizontal tail - longitudinal characteristics
Author:
Graham, David
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A51H10a
Link:
https://digital.library.unt.edu/ark:/67531/metadc59006/
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