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Some Effects of Wing Height on the Vertical-Tail Pressure Distributions of a Complete Model in Sideslip at High Subsonic Speeds
Author:
Few, Albert G., Jr.
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L57D22
Link:
https://digital.library.unt.edu/ark:/67531/metadc63687/
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