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Wind-tunnel investigation at high subsonic speeds of the effect of spoiler profile on the lateral control characteristics of a wing-fuselage combination winter quarter-chord line swept back 32.6©� and NACA 65A006 airfoil section

Wind-tunnel investigation at low speed of the effect of varying the ratio of body diameter to wing span from 0.1 to 0.8 on the aerodynamic characteristics in pitch of the 45©� sweptback-wing--body combination

Published Year

• 1950-1959 (2)

Subject

• Airplanes--Wings, Swept-back (2) *
• Stability of airplanes, Lateral (1)

Author

• Johnson, Harold S. (2) *

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