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Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4

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

Published Year

• 1950-1959 (2)

Subject

• Airplanes--Wings, Swept-back--Handling characteristics (2) *
• Airplanes--Fuselage (1)
• Mach number (1)
• Spoilers (Airplanes)--Performance (1)

Author

• Bingham, Gene J. (1)
• Braslow, Albert L. (1)
• Fields, E. M. (1)
• Schult, Eugene D. (1)

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