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By referring to FIGURE 1 determine the following: The reaction forces at supports B and D. Draw the shear force diagram for the beam. Calculate the coordinates of the centroid of the lamina shown in FIGURE 2.

Physics

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Answer

RB=38.05 kNR_B = \text{38.05 kN}

RD=62.95 kNR_D = \text{62.95 kN}

(42.31 mm,31.54 mm)(42.31 \text{ mm}, 31.54 \text{ mm})

Step-by-step solution

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here are the solutions to Question 5.

QUESTION 5: STATICS

5.1

A simply supported beam is loaded as shown in FIGURE 1.

5.1.1 The reaction forces at supports B and D.
  1. Convert the distributed load into an equivalent point load.

    The distributed load is 6 kN/m6 \text{ kN/m} over 3.5 m3.5 \text{ m}.
    Equivalent point load Fw=6 kN/m×3.5 m=21 kNF_w = 6 \text{ kN/m} \times 3.5 \text{ m} = 21 \text{ kN}.
    This load acts at the center of the distributed load, which is 1.5 m+3.5 m2=1.5 m+1.75 m=3.25 m1.5 \text{ m} + \frac{3.5 \text{ m}}{2} = 1.5 \text{ m} + 1.75 \text{ m} = 3.25 \text{ m} from point A.

  2. Apply the equilibrium equation for the sum of vertical forces.

    Let RBR_B and RDR_D be the upward reaction forces at supports B and D, respectively. Upward forces are positive, downward forces are negative.

    ∑Fy=0\sum F_y = 0 RB+RD−18 kN−21 kN−40 kN−22 kN=0R_B + R_D - 18 \text{ kN} - 21 \text{ kN} - 40 \text{ kN} - 22 \text{ kN} = 0 RB+RD−101 kN=0R_B + R_D - 101 \text{ kN} = 0 RB+RD=101 kN(1)R_B + R_D = 101 \text{ kN} \quad (1)
  3. Apply the equilibrium equation for the sum of moments about support B.

    Taking moments about B (clockwise moments are positive):
    The distance from A to B is 1.5 m1.5 \text{ m}.
    The distance from the equivalent point load FwF_w to B is 3.25 m−1.5 m=1.75 m3.25 \text{ m} - 1.5 \text{ m} = 1.75 \text{ m}.
    The distance from the 40 kN40 \text{ kN} load to B is 5 m−1.5 m=3.5 m5 \text{ m} - 1.5 \text{ m} = 3.5 \text{ m}.
    The distance from D to B is 6.5 m−1.5 m=5 m6.5 \text{ m} - 1.5 \text{ m} = 5 \text{ m}.
    The distance from the 22 kN22 \text{ kN} load to B is 9 m−1.5 m=7.5 m9 \text{ m} - 1.5 \text{ m} = 7.5 \text{ m}.

    ∑MB=0\sum M_B = 0 (−18 kN×1.5 m)+(21 kN×1.75 m)+(40 kN×3.5 m)−(RD×5 m)+(22 kN×7.5 m)=0(-18 \text{ kN} \times 1.5 \text{ m}) + (21 \text{ kN} \times 1.75 \text{ m}) + (40 \text{ kN} \times 3.5 \text{ m}) - (R_D \times 5 \text{ m}) + (22 \text{ kN} \times 7.5 \text{ m}) = 0 −27+36.75+140−5RD+165=0-27 + 36.75 + 140 - 5R_D + 165 = 0 314.75−5RD=0314.75 - 5R_D = 0 5RD=314.755R_D = 314.75 RD=314.755=62.95 kNR_D = \frac{314.75}{5} = 62.95 \text{ kN}
  4. Calculate RBR_B using Equation (1).

    RB+62.95 kN=101 kNR_B + 62.95 \text{ kN} = 101 \text{ kN} RB=101 kN−62.95 kN=38.05 kNR_B = 101 \text{ kN} - 62.95 \text{ kN} = 38.05 \text{ kN}

    The reaction forces are:
    RB=38.05 kNR_B = \boxed{\text{38.05 kN}}
    RD=62.95 kNR_D = \boxed{\text{62.95 kN}}

    5.1.2 Draw the shear force diagram for the beam.

    To draw the shear force diagram, we calculate the shear force at key points along the beam.

    • At A (x = 0 m):
      • Just right of 18 kN load: VA=−18 kNV_A = -18 \text{ kN}
    • From A to B (0 m < x < 1.5 m):
      • Shear force is constant: V=−18 kNV = -18 \text{ kN}
    • At B (x = 1.5 m):
      • Just left of RBR_B: V=−18 kNV = -18 \text{ kN}
      • Just right of RBR_B: V=−18 kN+38.05 kN=20.05 kNV = -18 \text{ kN} + 38.05 \text{ kN} = 20.05 \text{ kN}
    • From B to 5 m (1.5 m < x < 5 m):
      • Distributed load of 6 kN/m6 \text{ kN/m} acts downwards. Shear force decreases linearly.
      • Shear force at 5 m (just left of 40 kN load): V5m,L=20.05 kN−(6 kN/m×3.5 m)=20.05 kN−21 kN=−0.95 kNV_{5m, L} = 20.05 \text{ kN} - (6 \text{ kN/m} \times 3.5 \text{ m}) = 20.05 \text{ kN} - 21 \text{ kN} = -0.95 \text{ kN}
      • The shear force crosses zero at x=1.5 m+20.05 kN6 kN/m≈1.5 m+3.34 m=4.84 mx = 1.5 \text{ m} + \frac{20.05 \text{ kN}}{6 \text{ kN/m}} \approx 1.5 \text{ m} + 3.34 \text{ m} = 4.84 \text{ m} from A.
    • At 5 m (x = 5 m):
      • Just left of 40 kN load: V=−0.95 kNV = -0.95 \text{ kN}
      • Just right of 40 kN load: V=−0.95 kN−40 kN=−40.95 kNV = -0.95 \text{ kN} - 40 \text{ kN} = -40.95 \text{ kN}
    • From 5 m to D (5 m < x < 6.5 m):
      • Shear force is constant: V=−40.95 kNV = -40.95 \text{ kN}
    • At D (x = 6.5 m):
      • Just left of RDR_D: V=−40.95 kNV = -40.95 \text{ kN}
      • Just right of RDR_D: V=−40.95 kN+62.95 kN=22 kNV = -40.95 \text{ kN} + 62.95 \text{ kN} = 22 \text{ kN}
    • From D to E (6.5 m < x < 9 m):
      • Shear force is constant: V=22 kNV = 22 \text{ kN}
    • At E (x = 9 m):
      • Just left of 22 kN load: V=22 kNV = 22 \text{ kN}
      • Just right of 22 kN load: V=22 kN−22 kN=0 kNV = 22 \text{ kN} - 22 \text{ kN} = 0 \text{ kN}

    Shear Force Diagram Description:

    • Start at −18 kN-18 \text{ kN} at point A.
    • Draw a horizontal line from A to B (at x=1.5 mx=1.5 \text{ m}) at −18 kN-18 \text{ kN}.
    • At B, draw a vertical line upwards to 20.05 kN20.05 \text{ kN}.
    • From B to x=5 mx=5 \text{ m}, draw a linearly decreasing line from 20.05 kN20.05 \text{ kN} to −0.95 kN-0.95 \text{ kN}. This line crosses the zero axis at approximately x=4.84 mx=4.84 \text{ m}.
    • At x=5 mx=5 \text{ m}, draw a vertical line downwards to −40.95 kN-40.95 \text{ kN}.
    • Draw a horizontal line from x=5 mx=5 \text{ m} to D (at x=6.5 mx=6.5 \text{ m}) at −40.95 kN-40.95 \text{ kN}.
    • At D, draw a vertical line upwards to 22 kN22 \text{ kN}.
    • Draw a horizontal line from D to E (at x=9 mx=9 \text{ m}) at 22 kN22 \text{ kN}.
    • At E, draw a vertical line downwards to 0 kN0 \text{ kN}.

    5.2

    Calculate the coordinates of the centroid of the lamina shown in FIGURE 2.

  5. Divide the lamina into simple geometric shapes and a hole.

    We can consider the lamina as two rectangles (Rectangle 1 and Rectangle 2) and subtract a rectangular hole (Hole 3).

    • Rectangle 1 (Vertical part):
      • Dimensions: 40 mm×80 mm40 \text{ mm} \times 80 \text{ mm}
      • Area A1=40×80=3200 mm2A_1 = 40 \times 80 = 3200 \text{ mm}^2
      • Centroid x1=402=20 mmx_1 = \frac{40}{2} = 20 \text{ mm}
      • Centroid y1=802=40 mmy_1 = \frac{80}{2} = 40 \text{ mm}
    • Rectangle 2 (Horizontal part, to the right of Rectangle 1):
      • Dimensions: (100−40) mm×40 mm=60 mm×40 mm(100 - 40) \text{ mm} \times 40 \text{ mm} = 60 \text{ mm} \times 40 \text{ mm}
      • Area A2=60×40=2400 mm2A_2 = 60 \times 40 = 2400 \text{ mm}^2
      • Centroid x2=40+602=40+30=70 mmx_2 = 40 + \frac{60}{2} = 40 + 30 = 70 \text{ mm}
      • Centroid y2=402=20 mmy_2 = \frac{40}{2} = 20 \text{ mm}
    • Hole 3 (Rectangular hole):
      • Dimensions: 20 mm×20 mm20 \text{ mm} \times 20 \text{ mm}
      • Area A3=20×20=400 mm2A_3 = 20 \times 20 = 400 \text{ mm}^2 (This area will be subtracted)
      • Centroid x3=20+202=30 mmx_3 = 20 + \frac{20}{2} = 30 \text{ mm}
      • Centroid y3=20+202=30 mmy_3 = 20 + \frac{20}{2} = 30 \text{ mm}
  6. Calculate the total area of the lamina.

    Atotal=A1+A2−A3A_{total} = A_1 + A_2 - A_3 Atotal=3200 mm2+2400 mm2−400 mm2=5200 mm2A_{total} = 3200 \text{ mm}^2 + 2400 \text{ mm}^2 - 400 \text{ mm}^2 = 5200 \text{ mm}^2
  7. Calculate the x-coordinate of the centroid (xˉ\bar{x}).

    xˉ=A1x1+A2x2−A3x3Atotal\bar{x} = \frac{A_1 x_1 + A_2 x_2 - A_3 x_3}{A_{total}} xˉ=(3200 mm2)(20 mm)+(2400 mm2)(70 mm)−(400 mm2)(30 mm)5200 mm2\bar{x} = \frac{(3200 \text{ mm}^2)(20 \text{ mm}) + (2400 \text{ mm}^2)(70 \text{ mm}) - (400 \text{ mm}^2)(30 \text{ mm})}{5200 \text{ mm}^2} xˉ=64000+168000−120005200 mm\bar{x} = \frac{64000 + 168000 - 12000}{5200} \text{ mm} xˉ=2200005200 mm=55013 mm≈42.31 mm\bar{x} = \frac{220000}{5200} \text{ mm} = \frac{550}{13} \text{ mm} \approx 42.31 \text{ mm}
  8. Calculate the y-coordinate of the centroid (yˉ\bar{y}).

    yˉ=A1y1+A2y2−A3y3Atotal\bar{y} = \frac{A_1 y_1 + A_2 y_2 - A_3 y_3}{A_{total}} yˉ=(3200 mm2)(40 mm)+(2400 mm2)(20 mm)−(400 mm2)(30 mm)5200 mm2\bar{y} = \frac{(3200 \text{ mm}^2)(40 \text{ mm}) + (2400 \text{ mm}^2)(20 \text{ mm}) - (400 \text{ mm}^2)(30 \text{ mm})}{5200 \text{ mm}^2} yˉ=128000+48000−120005200 mm\bar{y} = \frac{128000 + 48000 - 12000}{5200} \text{ mm} yˉ=1640005200 mm=41013 mm≈31.54 mm\bar{y} = \frac{164000}{5200} \text{ mm} = \frac{410}{13} \text{ mm} \approx 31.54 \text{ mm}

    The coordinates of the centroid of the lamina are (42.31 mm,31.54 mm)\boxed{(42.31 \text{ mm}, 31.54 \text{ mm})}.

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