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A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36©�

Lift-curve slopes determined in flight on a flexible swept-wing jet bomber

A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring

Heat transfer to bodies at angles of attack

Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet

Published Year

• 1950-1959 (5) *

Subject

• Angle of attack (Aerodynamics) (5) *
• Charts, diagrams, etc (3)
• Aerodynamic load (2)
• Airplanes--Wings, Swept-back (2)
• Acceleration (Mechanics)--Measurement (1)
• Aeronautics--Research (1)
• Airplanes, Military--Bombers (1)
• Airplanes--Flight testing (1)
• Airplanes--Fuselage (1)
• Airplanes--Motors--Cowlings (1)
• Airplanes--Nacelles (1)
• Airplanes--Tail surfaces (1)
• Body of revolution (1)
• Butteting (Aerodynamics) (1)
• Diffusers (1)
• Heat--Transmission (1)
• Jet engines--Air intakes (1)
• Leading edges (Aerodynamics) (1)
• Lift (Aerodynamics) (1)

Author

• Aiken, William S., (1)
• Beheim, Milton A. (1)
• Cooper, Morton. (1)
• Feller, William V. (1)
• Fisher, Raymond A. (1)
• Gapcynski, John P. (1)
• Hasel, Lowell E. (1)
• Lautenberger, J. Walter, (1)
• Piercy, Thomas G. (1)
• Sutton, Fred B. (1)

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