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Investigation of the NACA 4-(4)(06)-04 two-blade propeller at forward Mach numbers to 0.925

An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47©� sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel

Published Year

• 1940-1949 (1)
• 1950-1959 (1)

Subject

• Charts, diagrams, etc (2)
• Lift (Aerodynamics) (2) *
• Wind tunnel testing (2)
• Aerodynamics, Transonic (1)
• Airplanes--Fuselage (1)
• Airplanes--Wings, Swept-back (1)
• Compressibility (1)
• Drag (Aerodynamics) (1)
• Propellers, Aerial--Testing (1)

Author

• Harrison, Daniel E. (2) *
• Bielat, Ralph P. (1)
• Coppolino, Domenic A. (1)
• Delano, James B. (1)

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