- 2067 Asar · 15 marks
Consistent deformation: frame, BMD, SFD, normal thrust
Short answer
Release fixed D and impose zero displacements there. Results: H_D=2.40 kN left, V_D=1.84 kN up, M_D=3.83 kNm anticlockwise; moments M_A=-4.90, M_B=-1.33, M_C=-3.38 kNm; axial compressions are AB 1.16, BC 2.40, CD 1.84 kN.
Use the consistent deformation method to solve the frame and draw bending moment, shear force and normal thrust diagrams. [Figure: frame; left column (2I) of 6 m, fixed base, carrying 1 kN/m UDL horizontally; beam (2I) of 6 m with 3 kN at 3 m from the left; right column (I) of 3 m, fixed base.]
Assumptions: A(0,0) and D are fixed bases. Column AB (2I) is 6 m high, beam BC (2I) is 6 m and column CD (I) is 3 m high, so D is 3 m above the level of A. The 1 kN/m UDL acts horizontally to the right on AB; the 3 kN load acts downward at 3 m from B on BC. Axial deformation is ignored. Positive bending moment = tension on the inside of the frame.
Degree of indeterminacy
Reactions: 3 + 3 = 6; equations = 3, so . Release the fixed support D. The redundants are (right +), (up +) and (anticlockwise +). The primary structure is a cantilever fixed at A.
Moments in the primary structure (kNm; for unit )
| Section | (H=1) | (V=1) | (M=1) | |
|---|---|---|---|---|
| A (AB) | -3.00 | 6.00 | 1.00 | -27.00 |
| B (AB) | 3.00 | 6.00 | 1.00 | -9.00 |
| B (BC) | 3.00 | 6.00 | 1.00 | -9.00 |
| C (BC) | 3.00 | 0.00 | 1.00 | 0.00 |
| C (CD) | 3.00 | 0.00 | 1.00 | 0.00 |
| D (CD) | 0.00 | 0.00 | 1.00 | 0.00 |
Flexibility matrix and load displacements ()
(For example .)
Consistent deformation (D is fixed: all three displacements are zero)
So kN to the left, kN upward, kNm anticlockwise.
Reactions at A (equilibrium)
kN (left), kN (up), kNm (anticlockwise). Check: ✓, ✓.
Bending moment diagram (, kNm; + inside tension)
| Section | BM |
|---|---|
| A | -4.90 |
| Mid-height of AB (3 m) | 1.38 |
| B | -1.33 |
| Under 3 kN load (BC) | 2.14 |
| C | -3.38 |
| D | 3.83 |
AB bends in a parabola (UDL); BC is two straight lines with a peak under the load; CD is a straight line with a change of sign.
Shear force and normal thrust
| Member | Axial N (+ tension) | Shear at start | Shear at end |
|---|---|---|---|
| AB | -1.16 | 3.60 | -2.40 |
| BC | -2.40 | 1.16 | -1.84 |
| CD | -1.84 | 2.40 | 2.40 |
Shear sign: positive when the force on the start end of the member acts along its local y-axis (90° anticlockwise from the direction A to B, B to C, C to D). Axial: negative = compression. Normal thrust in AB, BC, CD is therefore 1.16, 2.40 and 1.84 kN compression. The shear in AB goes from 3.60 kN at A to -2.40 kN at B (linear, due to the UDL), and in BC it is 1.16 kN before the 3 kN load and -1.84 kN after it.
Answer: kN, kN, kNm; , , kNm (inside tension +).
✓ Answer checked by Claude Opus 5.5 (high effort)
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