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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