(SEM V) THEORY EXAMINATION 2024-25 STRUCTURAL ANALYSIS
B.Tech
Data Structure
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Subject Code: BCE502 Maximum Marks: 70 Time: 3 Hours Paper ID: 310458
Question Paper Overview
SECTION A (2 × 7 = 14 Marks)
(Short theoretical questions — definitions, principles, and basic concepts)
a. Classify structures based on stability. b. Where should loads be applied on a pin-jointed truss? c. Give the classification of trusses. d. List the assumptions made while finding forces in a truss. e. What is the use of Maxwell’s Reciprocal Theorem? f. State the advantages of Influence Line Diagrams (ILDs). g. Explain the principle of Eddy’s Theorem.
SECTION B (Attempt any three × 7 = 21 Marks)
(Medium-length derivation or application-based problems)
a. Determine the degree of indeterminacy of the truss shown in figure. b. Explain simple trusses (with sketch) that are stable in form independent of support conditions. c. A continuous beam ABC of equal spans l undergoes settlement:
Support B sinks by δ₁, and support C sinks by δ₂.
Find reactions using the strain energy method. d. A UDL of 15 kN/m (3 m long) crosses a 10 m span girder — find the maximum shear force (S.F.) and bending moment (B.M.) at a section 4 m from the left support. e. Formulate the equations for a three-hinged parabolic arch and a three-hinged circular arch.
SECTION C (Attempt one part from each question × 7 = 35 Marks)
Q3
(a) Define static indeterminacy and give at least two examples in trusses. OR (b) A cable of 100 m span with ends 8 m above its lowest point carries a UDL of 10 kN/m.
Find horizontal and vertical reactions at supports and the length of cable.
Q4
(a) For a Warren-type cantilever truss, determine member forces using the method of tension coefficients. OR (b) State the conditions for zero-force members in a truss.
Q5
(a) A simply supported beam (6 m) has a 45 kN load at 2 m from left support.
Find deflection under the load using unit load method.
Take E = 200×10⁶ kN/m² and I = 14×10⁻⁶ m⁴. OR (b) A beam ABCD (30 m) is simply supported at A and D, with I-values:
I₁ = I (AB = 10 m),
I₂ = 3I (BC = 10 m),
I₃ = 2I (CD = 10 m).
Loads: 150 kN at B, 300 kN at C.
Using Conjugate Beam Method, determine slopes and deflections at A, B, C, D.
Given: E = 200 kN/mm², I = 2×10¹⁰ mm⁴.
Q6
(a) Explain Müller–Breslau’s Principle and verify with an example. OR (b) Draw influence line diagrams (ILDs) for S.F. and B.M. at a section 3 m from left end of a 12 m simply supported beam, and determine max S.F. and max B.M. due to a 5 m UDL of 2 kN/m.
Q7
(a) Define normal thrust and radial shear force for three-hinged arches. Derive expressions for both. OR (b) A three-hinged parabolic arch (span = 20 m, rise = 4 m) carries UDL = 20 kN/m on half span.
Find maximum bending moment for the arch.
Key Topics for Revision
1. Classification of Structures
Based on stability:
Stable, Unstable, Determinate, Indeterminate.
Static determinacy condition:
Ds=r+m−2jD_s = r + m - 2jDs=r+m−2j
where rrr = reactions, mmm = members, jjj = joints.
2. Trusses
Loads in truss: Applied only at joints (assumed pin-connected).
Types: Simple, Compound, Complex.
Assumptions:
Members are pin-jointed.
Loads act only at joints.
Self-weight neglected.
Members carry only axial force (tension or compression).
Zero-force members:
At a joint with two non-collinear members & no load, both are zero-force.
At a joint with three members and two are collinear, the third is zero-force.
3. Maxwell’s Reciprocal Theorem
States that:
δAB=δBA\delta_{AB} = \delta_{BA}δAB=δBA
Deflection at point A due to unit load at B = deflection at B due to unit load at A.
Used in flexibility methods.
4. Influence Line Diagrams (ILDs)
Show variation of internal forces (S.F., B.M., reaction) at a specific point as a unit load moves across the structure.
Applications: Analysis of moving loads, bridges, cranes, etc.
Advantages:
Determine max values under any moving load.
Essential for bridge and railway design.
5. Theorems of Structural Analysis
Eddy’s Theorem: Relation between strain energy and deflection.
Müller–Breslau’s Principle: Shape of ILD for a function = deflected shape of structure when that function is given a unit displacement.
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