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Rocket-Model Investigation of Hinge-Moments on a Trailing-Edge Control on a 52.5 Degree Swept Wing Between Mach Numbers of 0.70 and 1.80
Author:
Martz, C. William
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L57F04
Link:
https://digital.library.unt.edu/ark:/67531/metadc63478/
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