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Subsonic investigation of effects of body indentation on zero-lift drag characteristics of a 45©� sweptback wing-body combination with natural and fixed boundary-layer transition through a range of Reynolds number from 1 x 10⁶ to 8 x 10⁶

An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds

Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule

Published Year

• 1950-1959 (3)

Subject

• Airplanes--Fuselage (3) *
• Aerodynamics, Transonic (2)
• Airplanes--Wings, Swept-back (2)
• Airplanes--Wings, Swept-back--Handling characteristics (1)
• Airplanes--Wings--Design and construction (1)
• Charts, diagrams, etc (1)
• Drag (Aerodynamics) (1)
• Wind tunnel testing (1)

Author

• Braslow, Albert L. (3) *
• Howell, Robert R. (2)
• Bingham, Gene J. (1)
• Palmer, William E. (1)

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