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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