Aircraft Structures - ENG2011-N 2. a Calculate the second moment of area (Moment of Inertia) of a beam of cross-section

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Aircraft Structures Eng2011 N 2 A Calculate The Second Moment Of Area Moment Of Inertia Of A Beam Of Cross Section 1 (29.05 KiB) Viewed 15 times

Aircraft Structures - ENG2011-N 2. a Calculate the second moment of area (Moment of Inertia) of a beam of cross-section as shown in Figure Q2.1. 3/4" 5 Figure 22.1. b. The beam shown in Figure 22.2. is supported at 2 points, A and C. It is subjected to a point load of 5 kN at point B, midway between A and C, and to a distributed load between point and the end of the beam at D. This distributed load varies linearly between 20 kN/m at C and zero at point D. SKN 20 kN/m 1.5m 1.5m 4.5m Figure 22.2. Draw the shear force and bending moment diagrams for the beam, stating the magnitude of the shear force and bending moments at points A, B, C & D and at point E which is midway between C and D.