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Effects of Mach number up to 0.34 and Reynolds number up to 8,000,000 on the maximum lift coefficient of a wing of NACA 66-series airfoil sections

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

Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region

Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack

Low-speed static stability characteristics of a cambered-delta-wing model

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

Published Year

• 1950-1959 (6) *

Subject

• Airplanes--Models--Wings (6) *
• Charts, diagrams, etc (5)
• Airplanes--Models--Testing (4)
• Wind tunnel testing (4)
• Airplanes--Wings, Swept-back (2)
• Airplanes--Wings, Triangular (2)
• Flaps (Airplanes) (2)
• Aerodynamic load (1)
• Aerofoils (1)
• Aerofoils--Testing (1)
• Airplanes--Control (1)
• Airplanes--Control surfaces (1)
• Airplanes--WIngs, Triangular (1)
• Camber (Aerofoils) (1)
• Gust loads (1)
• Leading edges (Aerodynamics) (1)
• Lift (Aerodynamics) (1)
• Mach number (1)
• Reynolds number (1)
• Rolling (Aerodynamics) (1)
• Stability of airplanes (1)
• Stability of airplanes, Longitudinal (1)

Author

• Fitzpatrick, James E. (1)
• Furlong, G. Chester. (1)
• Jones, Robert A. (1)
• Knechtel, Earl D. (1)
• Lee, George. (1)
• McDearmon, Russell W. (1)
• Moseley, William C., (1)
• Pierce, Harold B. (1)
• Reisert, Thomas D. (1)
• Riebe, John M. (1)
• Thompson, Robert F. (1)

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