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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