k Evolution of the airfoil, 19081944. Creator Unknown. Evolution of the airfoil, 19081944. Diagrams showing the historical evolution of airfoil sections. The last two shapes are lowdrag sections designed to have laminar flow over 60 to 70 percent of chord on both the upper and lower surface. Examples illustrated include designs by the Wright Brothers, the Aerodynamics Research Institute in Gxf6ttingen, Louis Bleriot, the Royal Air Force, and the National Advisory Committee for Aeronautics. Editorial Stock Photo - Afloimages
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Evolution of the airfoil, 1908 1944.  Creator: Unknown. Evolution of the airfoil, 1908 1944. Diagrams showing the historical evolution of airfoil sections. The last two shapes are low drag sections designed to have laminar flow over 60 to 70 percent of chord on both the upper and lower surface. Examples illustrated include designs by the Wright Brothers, the Aerodynamics Research Institute in G  xf6 ttingen, Louis Bleriot, the Royal Air Force, and the National Advisory Committee for Aeronautics.
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Evolution of the airfoil, 1908-1944. Creator: Unknown.

Evolution of the airfoil, 1908-1944. Diagrams showing the historical evolution of airfoil sections. The last two shapes are low-drag sections designed to have laminar flow over 60 to 70 percent of chord on both the upper and lower surface. Examples illustrated include designs by the Wright Brothers, the Aerodynamics Research Institute in Göttingen, Louis Bleriot, the Royal Air Force, and the National Advisory Committee for Aeronautics.

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ID
172520341

Collection

License type
Editorial

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Creation date
23-10-2021

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