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Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60©� delta wing at Mach numbers from 0.75 to 1.96

Flight investigation of a small side-located control stick used with electronic control systems in a fighter airplane

Published Year

• 1950-1959 (2) *

Subject

• Airplanes--Control systems--Testing (2) *
• Airplanes--Wings, Triangular (1)
• Fighter planes--Flight testing (1)
• Hinge moments (Aerodynamics) (1)
• Trailing edge flaps (1)
• Trailing edges (Aerodynamics) (1)

Author

• Alford, William L. (1)
• Brown, Hoyt V. (1)
• Guy, Lawrence D. (1)
• Russell, Walter R. (1)
• Sjoberg, S. A. (1)

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