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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

Published Year

• 1950-1959 (1)

Subject

• Airplanes--Fuselage (1) *
• Airplanes--Wings, Swept-back--Handling characteristics (1)

Author

• Bingham, Gene J. (1) *
• Braslow, Albert L. (1)

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