Graphically position the links for the small aircraft nosewheel actuation mechanism shown in Figure P4.20. Then reposition the links as the 12-in. crank is rotated 60° clockwise from the orientation shown. Determine the resulting angular displacement of the wheel assembly. 32" 15° 5" 12" 26" 30" 30"

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Buckling of columns

The column is described as a vertical member of the structure that carries an axial compressive load, and buckling is a lateral deformation of the column under the application of load.