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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 Influence of a Change in Body Shape on the Effects of Twist and Camber as Determined by a Transonic Wind-Tunnel Investigation of a 45 Degree Sweptback Wing-Fuselage Configuration

Published Year

• 1950-1959 (2) *

Subject

• Aerodynamics, Transonic (1)
• Airplanes--Fuselage (1)
• Airplanes--Wings, Swept-back (1)
• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Wind tunnel testing (1)

Author

• Harrison, Daniel E. (2) *
• Bielat, Ralph P. (1)
• Coppolino, Domenic A. (1)

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