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Test of NACA 66,2-116, a =0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane

Wind tunnel investigation of control surface characteristics.12 - Various cover-plate alinements on the NACA 0015 airfoil with a 30 percent chord flap and large sealed internal balance

Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds

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

• 1940-1949 (2)
• 1950-1959 (2)

Subject

• Hinge moments (Aerodynamics) (4) *
• Charts, diagrams, etc (3)
• Wind tunnel testing (3)
• Airplanes--Control surfaces (2)
• Airplanes--Wings, Triangular (2)
• Flaps (Airplanes) (2)
• Trailing edges (Aerodynamics) (2)
• Aerodynamic load (1)
• Aerodynamics, Supersonic (1)
• Aerodynamics, Transonic (1)
• Aerofoils (1)
• Aerofoils--Testing (1)
• Airplanes--Control systems--Testing (1)
• Drag (Aerodynamics) (1)
• Flaps (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Plates (Engineering) (1)
• Trailing edge flaps (1)

Author

• Guy, Lawrence D. (2)
• Abbott, Frank T. (1)
• Brown, Hoyt V. (1)
• Hoggard, H. Page. (1)
• Underwood, William J. (1)

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