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Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35©�, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method

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 wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4

Recent control studies

Published Year

• 1950-1959 (4) *

Subject

• Flaps (Airplanes) (4) *
• Airplanes--Control surfaces (3)
• Charts, diagrams, etc (3)
• Airplanes--Models--Wings (2)
• Airplanes--Wings, Swept-back (2)
• Wind tunnel testing (2)
• Aerodynamics, Supersonic (1)
• Aerodynamics, Transonic (1)
• Aerofoils--Testing (1)
• Airplanes--Control (1)
• Airplanes--Models--Testing (1)
• Airplanes--Wings, Triangular (1)
• Hinge moments (Aerodynamics) (1)
• Leading edges (Aerodynamics) (1)
• Spoilers (Airplanes) (1)
• Stability of airplanes, Longitudinal (1)
• Trailing edges (Aerodynamics) (1)

Author

• Guy, Lawrence D. (1)
• Knechtel, Earl D. (1)
• Lee, George. (1)
• Lowry, John G. (1)
• Thompson, Robert F. (1)

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