Structural Analysis—I - B.Tech. Examination 2018
Structural Analysis—I
Instructions:
- The marks are indicated in the right‑hand margin.
- There are NINE questions in this paper.
- Attempt FIVE questions in all.
- Question No. 1 is compulsory.
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In case of conjugate beam the internal hinged is converted into which support?
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The ordinates of influence line diagram for bending moment always have dimension of
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A three‑hinged parabolic arch of span 20 and rise 5 carries UDL of intensity 15 kN/m over whole span, the value of bending moment at a section 5 m from left end is
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Flexibility matrix method is based on the
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In a simply supported beam, a load \(20 \mathrm{kN}\) is placed at \(A\) which is at a distance of \(6 \mathrm{m}\) from the left caused the deflection at \(B\) of \(10 \mathrm{mm}\). When the load is \(10 \mathrm{kN}\) at \(B\) which is same distance from the right end, then find the deflection at point \(A\).
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The Castigliano's theorem is applicable for the structures
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The degree of kinematic indeterminacy of a pin‑jointed space frame is given by
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The rate of change of bending moment in any structure is equal to the
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A cantilever beam of span \(L\) carries point load of intensity \(W \mathrm{kN}\) at the free end and another beam which is simply supported at both ends of length \(L\) carries point load \(W \mathrm{kN}\) at the center. What is the ratio of maximum deflection of cantilever beam to simply supported beam?
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The strain energy stored in the member due to bending per unit volume is given by
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Describe the differences between determine and indeterminate structures. Also determine static and kinematic indeterminacy of structures shown in Fig. 1.
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A three‑hinged parabolic arch ACB of span \(30\mathrm{m}\) has its left support at depth \(4\mathrm{m}\) and right support at depth \(16\mathrm{m}\) below the crown hinge C. The arch carries a point load of \(60\mathrm{kN}\) at a distance of \(5\mathrm{m}\) from left side of C and point load of \(120\mathrm{kN}\) at a distance of \(10\mathrm{m}\) from right side of C. Find the reaction at the supports and the bending moment under the loads.
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Three wheel loads \(60\mathrm{kN}\), \(40\mathrm{kN}\) and \(50\mathrm{kN}\) spaced at \(2\mathrm{m}\) and \(2\mathrm{m}\) respectively roll on girder of span \(20\mathrm{m}\) from left to right with the \(60\mathrm{kN}\) load leading. Find maximum and absolute maximum bending moment that can occur at a section \(6\mathrm{m}\) from the left support. Also determine maximum positive and negative shear force at that section.
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Find out horizontal and vertical deflections of point A of circular structure shown in Fig. 2, EI is constant :
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Derive and describe the Maxwell law of reciprocal deflection theorem and also its generalized form.
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A beam AB of length \(L\) simply supported at the ends carries a point load \(W\) at a distance from the left end and b distance from right end. Find the deflection under the load and the maximum deflection.
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A three‑hinged parabolic arch ACB of span \(30\mathrm{m}\) has its left support at depth \(4\mathrm{m}\) and right support at depth \(16\mathrm{m}\) below the crown hinge C. The arch carries a point load of \(60\mathrm{kN}\) at a distance of \(5\mathrm{m}\) from left side of C and point load of \(120\mathrm{kN}\) at a distance of \(10\mathrm{m}\) from right side of C. Find the reaction at the supports and the bending moment under the loads.
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Find the forces in each member by method of tension coefficient of the Fig. 3 :
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A cable is supported between two points \(40 \mathrm{m}\) horizontal apart. The left support is \(5 \mathrm{m}\) above the right support. The cable carries a load of \(6 \mathrm{kN / m}\) on the horizontal span. The lowest point of cable is \(5 \mathrm{m}\) below the left support. Find the maximum tension in the cable.
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Draw the influence line diagram of the structure as shown in Fig. 4 for reaction at \(A\), reaction at \(B\), shear force and bending moment at section \(E\). Also find the ordinates of influence line diagrams.
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Find vertical deflection, horizontal deflection and slope at end \(A\) of the frame member ABCD shown in Fig. 5. Take \(E = 210 \mathrm{kN / mm^2}\), \(I_{AC} = 4 \times 10^7 \mathrm{mm^4}\) and \(I_{CD} = 8 \times 10^7 \mathrm{mm^4}\).
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What is the difference between flexibility matrix and stiffness matrix? Discuss in detail.
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Determine the stiffness matrix of the structure shown in Fig. 6 :