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Static longitudinal characteristics at high subsonic speeds of a complete airplane model with a highly tapered wing having the 0.80 chord line unswept and with several tail configurations
Author:
Goodson, Kenneth W
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56J03
Link:
https://digital.library.unt.edu/ark:/67531/metadc62881/
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