Sample Test1_10

Sample Test1_10 - CLARKSON UNIVERSITY Department of...

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CLARKSON UNIVERSITY Department of Mechanical and Aeronautical Engineering AE/ME 350 Aircraft Structural Analysis (Fall 2010) Sample Test #1 Closed book Closed notes Time : 1:15 hour 1. List the five main requirements/design criteria for aircraft structural design? (5) 2. Consider a point in an elastic body located at ( x = 5, y = 0, z = 0 ). A load applied to the body causes a displacement of the point in the x -direction given by u = 0.02x + 0.02y – 0.01z. Determine the x -location of the point after deformation (load application). (5) 3. Consider a constant shear flow q on a closed thin-walled section of arbitrary shape as shown in Fig. 1. Show that the resultant torque 2 TA q , where A = Area enclosed by the shear flow. (5) q x y 4. A solid shaft of circular cross-section supports a torque of 50 kNm and a bending
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Sample Test1_10 - CLARKSON UNIVERSITY Department of...

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