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Five structural engineering questions from an exam held at cork institute of technology in summer 2005. The questions involve determining joint displacements, bending moments, deflections, and reactions for various frames and plates using the stiffness matrix method and other structural analysis techniques. The document also includes stability coefficients for use in determining critical loads for frames.
Typology: Exams
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(NFQ – Level 8)
Instructions Answer any FIVE questions. All questions carry equal marks.
Examiners: Mr. J. J. Murphy Mr. T. Corcoran Prof. P. O’Donoghue
Q1. The uniform frame shown in Fig Q1 has rigid joints at D and E and fixed foundation connections at A and B. It is pinned to the support at C. (a) Use the stiffness matrix method to determine the joint displacements at C, D and E. (b) Determine the bending moments at A, B, D and E and hence draw the bending moment diagram for the frame, noting all significant values. Axial and shear deformations may be neglected. E= 205 kN/mm^2 I = 10^7 mm^4
Q2. The symmetrical pin-jointed steel framework shown in Fig. Q2 is pinned to supports at A and B. The cross-sectional area of each member is 800 mm^2. Member DE is subjected to an increase of temperature of 40 K and a vertical force of 40 kN is applied at D (a) Use the stiffness matrix method to determine the vertical deflections at C, D and E. (b) Determine the resulting forces in each of the members. (c) Determine the horizontal and vertical reactions at A and B. E = 205 kN/mm^2 α = 12 x 10-6^ K -
Q3. A thin elastic rectangular plate of length 2 l and width l and uniform flexural rigidity D is simply supported along its edges. It is subjected to a load p = - p o Cos(πx/2 l ) Cos(πy/ l ), where x and y are rectangular coordinates measured from the origin at the centre of the plate as shown in Fig. Q3. Derive an expression for the deflection of the plate and hence determine: (i) the maximum value of M (^) x in the plate, (ii) the maximum value of M (^) y in the plate, (iii) the maximum value of the twisting moment Mxy in the plate, (iv) the vertical reactions at the corner of the plate, (v) the maximum value of Qy along the edge y = l /2. ν = 0.
Q4. (a) A steel rail section for which E = 205 kN/mm^2 and I = 12000 cm^4 is supported on sleepers, ballast and road bed, which together behave approximately as a beam on an elastic foundation for which k = 5 MN/m^2. If the rail is subjected to two wheel loads of 150 kN spaced 1.2 m apart along the rail (see Fig. Q4(a)), determine the maximum deflection of the rail and the maximum bending moment in the rail. (12 marks) (b) Use qualitative analysis to sketch the bending moment diagrams and the deflected shapes for the frames shown in Fig. Q4(b). Indicate also the direction in which the reactions act. (8 marks) Use Answer sheet provided
Q5. (a) Fig. Q5(a) shows a frame, which is fixed to a support at A and pinned to a support at B. The beam CD has a mass of 12000 kg and may be assumed to be infinitely stiff. The flexural rigidity of each column is the same at 8 MNm^2 and the mass of the columns may be neglected. Calculate the fundamental natural mode frequency of the frame and hence determine the maximum horizontal deflection of point C when the beam CD is subjected to a sinusoidally varying horizontal load of frequency 2 hz and amplitude 12 kN, if the damping coefficient ξ = 0.06. (10 marks) (b) Fig Q5(b) shows a two-storey portal frame fixed to a support at A and pinned to a support at F. The beams may be assumed to be infinitely stiff and to have masses 15000 kg and 5000 kg as shown. The columns are of uniform stiffness with EI = 12 MNm^2. The mass of the columns may be neglected. Calculate the natural mode frequencies of the frame. (10 marks)