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Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method

Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick tapered, unswept wing

Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds

Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds

Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered winds at transonic speeds

Longitudinal characteristics of wings

Published Year

• 1940-1949 (1)
• 1950-1959 (5)

Subject

• Airplanes--Wings (6) *
• Airplanes--Fuselage (2)
• Charts, diagrams, etc (2)
• Drag (Aerodynamics) (2)
• Aerodynamics, Supersonic (1)
• Aerodynamics, Transonic (1)
• Ailerons (1)
• Air flow (1)
• Airplanes--Control surfaces (1)
• Airplanes--Design and construction (1)
• Airplanes--Fuel tanks (1)
• Airplanes--Tail surfaces (1)
• Airplanes--WIngs (1)
• Aspect ratio (Aerofoils) (1)
• Lift (Aerodynamics) (1)
• Pitching (Aerodynamics) (1)
• Rolling (Aerodynamics) (1)
• Spoilers (Airplanes) (1)
• Stability of airplanes, Lateral (1)

Author

• Malvestuto, Frank S. (2)
• Alford, William J. (1)
• Bobbitt, Percy J. (1)
• English, Roland D. (1)
• Hammond, Alexander D. (1)
• Huffman, Jarrett K. (1)
• Margolis, Kenneth. (1)
• Morrison, William D. (1)
• Sleeman, William C. (1)
• Toll, Thomas A. (1)

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