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- An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47©� sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel
- The effective downwash characteristics at transonic speeds of a 6-percent-thick wing with 47 degrees of sweepback in combination with a cylindrical body as determined from force measurements of a horizontal tail