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While using three moments equation, a fixed end of a continuous beam is replaced by an additional span of

A. Zero length

B. Infinite length

C. Zero moment of inertia

D. None of the above

Answer: Option A

Solution (By Examveda Team)

The three-moment equation is used for the analysis of continuous beams. When one end of a continuous beam is fixed, an imaginary or fictitious span is introduced beyond the fixed end so that the three-moment equation can be applied.

For a fixed end, this additional imaginary span is assumed to have zero length. This allows the fixed-end condition of zero rotation (zero slope) to be incorporated into the three-moment equation.

Option A: Zero length
Correct. A fixed end is represented by an imaginary span of zero length when applying the three-moment equation.

Option B: Infinite length
Incorrect. An infinite-length span is not used to represent a fixed end in the three-moment equation.

Option C: Zero moment of inertia
Incorrect. Zero moment of inertia would imply zero flexural stiffness and does not represent a fixed-end condition.

Option D: None of the above
Incorrect because Option A correctly represents the fixed end.

Hence, Option A — Zero length is the correct answer.

This Question Belongs to Civil Engineering >> Structural Analysis

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Comments (3)

  1. CHANDU
    CHANDU :
    2 weeks ago

    Explanation pls

  2. CHANDU
    CHANDU :
    2 weeks ago

    Explanation pls

  3. Atif Muneer
    Atif Muneer:
    7 years ago

    to overcome the concept of this question uh guys should study the three moment equation

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When a series of wheel loads crosses a simply supported girder, the maximum bending moment under any given wheel load occurs when

A. The centre of gravity of the load system is midway between the centre of span and wheel load under consi-deration

B. The centre of span is midway between the centre of gravity of the load system and the wheel load under consideration

C. The wheel load under consideration is midway between the centre of span and the centre of gravity of the load system

D. None of the above