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The effects of trailing-edge flaps on the subsonic aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3
Author:
Tinling, Bruce E.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A54L07
Link:
https://digital.library.unt.edu/ark:/67531/metadc62223/
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