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Q1. Find the centroidal axes, Moment of Inertia, and Polar moment of inertia of the section shown below. Q2a. Write briefly on the following: Proof Resilience, Strain Energy, Impact Loading, Modulus of Resilience, Obliquity and how it is determined, Principal plane, Mohr's Circle

Mathematics

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Answers

3 parts
a

(80 mm,130 mm)\text{}(80 \text{ mm}, 130 \text{ mm})\text{}

b

\text{}

c

\text{}

Step-by-step solution

3 steps

Here's the solution for Q1:

To solve this, we first divide the T-section into two rectangles: a flange (Rectangle 1) and a web (Rectangle 2). We'll establish a reference axis at the bottom-left corner of the section.

Step 1: Define the properties of each rectangular component.

  • Rectangle 1 (Flange):

    • Width (b1b_1) = 160 mm160 \text{ mm}
    • Height (h1h_1) = 40 mm40 \text{ mm}
    • Area (A1A_1) = b1×h1=160 mm×40 mm=6400 mm2b_1 \times h_1 = 160 \text{ mm} \times 40 \text{ mm} = 6400 \text{ mm}^2
    • Centroidal x-coordinate from left edge (x1x_1) = 160 mm2=80 mm\frac{160 \text{ mm}}{2} = 80 \text{ mm}
    • Centroidal y-coordinate from bottom reference (y1y_1) = 160 mm+40 mm2=180 mm160 \text{ mm} + \frac{40 \text{ mm}}{2} = 180 \text{ mm}
  • Rectangle 2 (Web):

    • Width (b2b_2) = 40 mm40 \text{ mm}
    • Height (h2h_2) = 160 mm160 \text{ mm}
    • Area (A2A_2) = b2×h2=40 mm×160 mm=6400 mm2b_2 \times h_2 = 40 \text{ mm} \times 160 \text{ mm} = 6400 \text{ mm}^2
    • Centroidal x-coordinate from left edge (x2x_2) = 80 mm80 \text{ mm} (since it's centered)
    • Centroidal y-coordinate from bottom reference (y2y_2) = 160 mm2=80 mm\frac{160 \text{ mm}}{2} = 80 \text{ mm}

Step 2: Calculate the centroidal axes (xˉ,yˉ\bar{x}, \bar{y}).

The total area A=A1+A2=6400 mm2+6400 mm2=12800 mm2A = A_1 + A_2 = 6400 \text{ mm}^2 + 6400 \text{ mm}^2 = 12800 \text{ mm}^2.

  • Centroidal x-coordinate (xˉ\bar{x}): Due to symmetry about the vertical axis, xˉ\bar{x} is at the center of the width.

    xˉ=160 mm2=80 mm\bar{x} = \frac{160 \text{ mm}}{2} = 80 \text{ mm}
  • Centroidal y-coordinate (yˉ\bar{y}):

    yˉ=A1y1+A2y2A1+A2\bar{y} = \frac{A_1 y_1 + A_2 y_2}{A_1 + A_2} yˉ=(6400 mm2×180 mm)+(6400 mm2×80 mm)12800 mm2\bar{y} = \frac{(6400 \text{ mm}^2 \times 180 \text{ mm}) + (6400 \text{ mm}^2 \times 80 \text{ mm})}{12800 \text{ mm}^2} yˉ=1152000 mm3+512000 mm312800 mm2\bar{y} = \frac{1152000 \text{ mm}^3 + 512000 \text{ mm}^3}{12800 \text{ mm}^2} yˉ=1664000 mm312800 mm2=130 mm\bar{y} = \frac{1664000 \text{ mm}^3}{12800 \text{ mm}^2} = 130 \text{ mm}

Part a· 2 steps

Centroidal axes

The centroid of the section is located at (xˉ,yˉ)=(80 mm,130 mm)(\bar{x}, \bar{y}) = \boxed{\text{}(80 \text{ mm}, 130 \text{ mm})\text{}} from the bottom-left corner.

  1. Calculate the Moment of Inertia about the centroidal x-axis (IxI_x).

    We use the parallel axis theorem: Ix=∑(Ixi+Aidyi2)I_x = \sum (I_{xi} + A_i d_{yi}^2), where Ixi=bihi312I_{xi} = \frac{b_i h_i^3}{12} and dyid_{yi} is the distance from the component's centroid to the overall centroidal x-axis.

    • For Rectangle 1 (Flange):

      • Ix1=160 mm×(40 mm)312=160×6400012=853333.33 mm4I_{x1} = \frac{160 \text{ mm} \times (40 \text{ mm})^3}{12} = \frac{160 \times 64000}{12} = 853333.33 \text{ mm}^4
      • dy1=y1−yˉ=180 mm−130 mm=50 mmd_{y1} = y_1 - \bar{y} = 180 \text{ mm} - 130 \text{ mm} = 50 \text{ mm}
      • A1dy12=6400 mm2×(50 mm)2=16000000 mm4A_1 d_{y1}^2 = 6400 \text{ mm}^2 \times (50 \text{ mm})^2 = 16000000 \text{ mm}^4
      • (Ix1+A1dy12)=853333.33+16000000=16853333.33 mm4(I_{x1} + A_1 d_{y1}^2) = 853333.33 + 16000000 = 16853333.33 \text{ mm}^4
    • For Rectangle 2 (Web):

      • Ix2=40 mm×(160 mm)312=40×409600012=13653333.33 mm4I_{x2} = \frac{40 \text{ mm} \times (160 \text{ mm})^3}{12} = \frac{40 \times 4096000}{12} = 13653333.33 \text{ mm}^4
      • dy2=yˉ−y2=130 mm−80 mm=50 mmd_{y2} = \bar{y} - y_2 = 130 \text{ mm} - 80 \text{ mm} = 50 \text{ mm}
      • A2dy22=6400 mm2×(50 mm)2=16000000 mm4A_2 d_{y2}^2 = 6400 \text{ mm}^2 \times (50 \text{ mm})^2 = 16000000 \text{ mm}^4
      • (Ix2+A2dy22)=13653333.33+16000000=29653333.33 mm4(I_{x2} + A_2 d_{y2}^2) = 13653333.33 + 16000000 = 29653333.33 \text{ mm}^4

    Total IxI_x:

    Ix=16853333.33 mm4+29653333.33 mm4=46506666.66 mm4I_x = 16853333.33 \text{ mm}^4 + 29653333.33 \text{ mm}^4 = 46506666.66 \text{ mm}^4
  2. Calculate the Moment of Inertia about the centroidal y-axis (IyI_y).

    Since the section is symmetrical about the y-axis, the centroidal y-axis passes through the centroid of each component, so dxi=0d_{xi} = 0. We sum the individual moments of inertia Iyi=hibi312I_{yi} = \frac{h_i b_i^3}{12}.

    • For Rectangle 1 (Flange):

      • Iy1=40 mm×(160 mm)312=40×409600012=13653333.33 mm4I_{y1} = \frac{40 \text{ mm} \times (160 \text{ mm})^3}{12} = \frac{40 \times 4096000}{12} = 13653333.33 \text{ mm}^4
    • For Rectangle 2 (Web):

      • Iy2=160 mm×(40 mm)312=160×6400012=853333.33 mm4I_{y2} = \frac{160 \text{ mm} \times (40 \text{ mm})^3}{12} = \frac{160 \times 64000}{12} = 853333.33 \text{ mm}^4

    Total IyI_y:

    Iy=13653333.33 mm4+853333.33 mm4=14506666.66 mm4I_y = 13653333.33 \text{ mm}^4 + 853333.33 \text{ mm}^4 = 14506666.66 \text{ mm}^4

Part b

\text{}

Moment of Inertia

The moment of inertia about the centroidal x-axis is 46.51×106 mm4\boxed{\text{}}46.51 \times 10^6 \text{ mm}^4\text{}.
The moment of inertia about the centroidal y-axis is 14.51×106 mm4\boxed{\text{}}14.51 \times 10^6 \text{ mm}^4\text{}.

  1. Calculate the Polar Moment of Inertia (JzJ_z).

    The polar moment of inertia about the centroid is the sum of the moments of inertia about the centroidal x and y axes:

    Jz=Ix+IyJ_z = I_x + I_y Jz=46506666.66 mm4+14506666.66 mm4J_z = 46506666.66 \text{ mm}^4 + 14506666.66 \text{ mm}^4 Jz=61013333.32 mm4J_z = 61013333.32 \text{ mm}^4

Part c

\text{}

Polar moment of inertia

The polar moment of inertia is 61.01×106 mm4\boxed{\text{}}61.01 \times 10^6 \text{ mm}^4\text{}.

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