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Autumn Examinations 2012 - Structural Engineering 1, Exams of Structural Analysis

The instructions and questions for the autumn examinations 2012 of the module 'structural engineering 1' in the bachelor of engineering in civil engineering program at cork institute of technology. Four questions related to determining support reactions, shear forces, bending moments, maximum bending stresses, centroid and second moment of area, plastic neutral axis, plastic section modulus, fatigue considerations, and column stresses and shortening.

Typology: Exams

2012/2013

Uploaded on 04/02/2013

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Download Autumn Examinations 2012 - Structural Engineering 1 and more Exams Structural Analysis in PDF only on Docsity! Page 1 of 3 CORK INSTITUTE OF TECHNOLOGY INSTITIÚID TEICNEOLAÍOCHTA CHORCAÍ Autumn Examinations 2012 Module Title: Structural Engineering 1 Module Code: CIVL 6024 School: Building & Civil Engineering Programme Title: Bachelor of Engineering in Civil Engineering – Year 2 Programme Code: CCIVL_7_Y2 External Examiner(s): Mr J. Murphy, Ms. M. Kyne Internal Examiner(s): Dr. R.A. Guinee, Mr. A. Conway Instructions: Please answer FOUR questions. All questions carry equal marks Duration: 2 Hours Sitting: Autumn 2012 Requirements for this examination: Note to Candidates: Please check the Programme Title and the Module Title to ensure that you have received the correct examination. If in doubt please contact an Invigilator. Page 2 of 3 Q1 (a) Determine the support reactions for the beam shown in Fig.Q1 (a) and hence draw the shear force and bending moment diagrams for the beam noting all significant values. Ignore point of contraflexture. (b) If the beam cross section is as shown in Fig.Q1 (b) determine the maximum tensile and compressive bending stresses in the beam. Q2 (a) Determine the force in each of the members of the pin jointed framework shown in Fig. Q2 using the method of joints. Indicate the forces on a neat sketch of the framework and show whether they are tensile or compressive. (b) If the above truss has an additional gravity load of 5kN at node C evaluate the forces in members 2, 3 and 4 using the method of sections Fig.Q1 (a) A B 6m 5m w = 20kN/m C W1 = 5kN 15kN 4m D W2 = 15kN 150mm  10mm 10mm  300mm 300mm  20mm Fig.Q1 (b) 1 2 3 4 5 A B C D Fig.Q2 10kN 2m 3m 1m 2m 2m 5kN
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