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A theoretical investigation of the dynamic lateral oscillatory stability of an airplane having a 60 degree triangular wing
Author:
Johnson, Joseph L.
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L9A04
Link:
https://digital.library.unt.edu/ark:/67531/metadc58196/
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