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Investigation at Low Speed of the Flow Field Behind the Lifting Surfaces of a Model Equipped With a 60 Degree Triangular Wing and a 60 Degree Triangular Canard Tail
Author:
Newman, Ernest E.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L53C30
Link:
https://digital.library.unt.edu/ark:/67531/metadc59721/
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