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Main points of this past exam are: Maximum Shear Stresses, Vertical Deflections, Equation for Bending Moment, Horizontal Deflection, Plane Pin-Jointed Framework, Principal Values, Flexural Shear Stress, Normal and Shear Stresses
Typology: Exams
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Instructions Answer any FIVE questions. All questions carry equal marks
Examiners: Mr. J. J. Murphy Prof. P. O’Donoghue Mr. P. Anthony
Q1. A plane pin-jointed framework is attached to a roller support at A and a pinned support at B and is loaded as shown in Fig. Q1. All the members are of steel and have cross- sectional areas of 1500 mm^2. Taking E = 205 kN/mm^2 determine the horizontal deflection of point C.
Q2. A uniform beam is loaded and supported as shown in Fig. Q2.
(a) Write the equation for the bending moment using Macaulay’s notation and hence determine the vertical deflections at C and D. (b) Draw the shear force and bending moment diagrams for the beam, noting the principal values (including all local maximum and minimum values). E = 205 kN/mm^2 I = 2000 cm^4
Q3. (a) Determine the horizontal and vertical reactions at A and G for the uniform two pinned
portal frame shown in Fig. Q3. (b) Draw the bending moment diagram for the frame, noting the principal values (at each load position).
Q4 A bi-metallic temperature sensitive component consists of a short steel tube of outside diameter 70 mm and internal diameter 60 mm fixed securely at its ends to a solid copper rod of 50 mm diameter as shown in Fig. Q4. At 15°C, the rod and cylinder have exactly the same length. If a 90 kN load is placed on top of the rod and cylinder, calculate the forces in the two materials if the whole assembly is heated to 55°C. Calculate also the temperature at which the copper would take all the force and the length of the component at this temperature. ESTEEL = 205 kN/mm^2 ECOPPER = 105 kN/mm^2 αSTEEL = 12 x 10-6^ /°C αCOPPER = 18 x 10-6^ /°C
Q5. A steel beam is loaded and supported as shown in Fig Q5(a). The cross-section of the beam is shown in Fig Q5(b). (a) Draw the shear force and bending moment diagrams for the beam, noting the principal values. (b) Determine the bending stress at point O on the cross-section (at the support, A). (c) Determine the flexural shear stress at O. (d) Determine the principal stresses at O. (e) Determine the maximum shear stresses at O. (f) Determine the normal and shear stresses on a plane at 35˚ to the vertical at O as shown in Fig Q5(c).
Q6.(a) A hollow aluminium tube of internal diameter 60 mm and external diameter 100 mm is securely connected at its ends to a solid steel bar of diameter 50 mm as shown in Fig. Q6. Determine the maximum torque that can be safely applied to the composite section if the limits of shear stress in the steel and aluminium are 75 N/mm^2 and 55 N/mm^2 respectively. (12 marks) (b) A solid steel shaft of diameter 150mm is subjected to a torque of 125 kNm. If the shear stress at yield is 165 N/mm^2 , determine the depth of yielding in the shaft and the angle of twist of a metre length of the shaft. If the shaft is subsequently unloaded, determine the residual stress on the outside surface of the shaft. (8 marks) GSTEEL= 80 kN/mm^2 GALUMINIUM = 26 kN/mm^2