Effects of vertical location of wing and horizontal tail on the aerodynamic characteristics in pitch at Mach numbers from 0.60 to 1.40 of an airplane configuration with an unswept wing

Stivers, Louis S., Jr., Lippmann, Garth W.
naca-rm-a57i10
1957


An investigation was conducted in the Ames 2- by2-foot transonic wind tunnel of a wing-body-tail combination.

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http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-a57i10.pdf