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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

Published Year

• 1950-1959 (1)

Subject

• Aerofoils--Testing (1)
• Airplanes--Control (1)
• Airplanes--Control surfaces (1)
• Airplanes--Models--Wings (1)
• Airplanes--Wings, Swept-back (1)
• Charts, diagrams, etc (1) *
• Flaps (Airplanes) (1)
• Wind tunnel testing (1)

Author

• Thompson, Robert F. (1) *

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