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Tests in the Ames 40- by 80-foot wind tunnel of an airplane model with an aspect ratio 4 triangular wing and an all-movable horizontal tail - high-lift devices and lateral controls
Author:
Franks, Ralph W
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A52K13
Link:
https://digital.library.unt.edu/ark:/67531/metadc59454/
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