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Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01
Author:
Robinson, Ross B
Year:
1958
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L58C18
Link:
https://digital.library.unt.edu/ark:/67531/metadc64112/
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