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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

Published Year

• 1950-1959 (1)

Subject

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

Author

• Brown, Hoyt V. (1) *
• Guy, Lawrence D. (1)

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