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Find the MOI about x:x & y:y axes

Physics

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Here's how to calculate the Moment of Inertia (MOI) for both shapes.

Shape 1: U-Channel

First, we divide the U-channel into three rectangles:

  • R1R_1: Bottom plate (width b1=70b_1 = 70 mm, height h1=10h_1 = 10 mm)
  • R2R_2: Left vertical plate (width b2=15b_2 = 15 mm, height h2=50h_2 = 50 mm)
  • R3R_3: Right vertical plate (width b3=15b_3 = 15 mm, height h3=50h_3 = 50 mm)
  1. Calculate the Centroid (xˉ,yˉ\bar{x}, \bar{y})

    We set the origin at the bottom-left corner.

    • A1=70×10=700 mm2A_1 = 70 \times 10 = 700 \text{ mm}^2, x1=35 mmx_1 = 35 \text{ mm}, y1=5 mmy_1 = 5 \text{ mm}
    • A2=15×50=750 mm2A_2 = 15 \times 50 = 750 \text{ mm}^2, x2=7.5 mmx_2 = 7.5 \text{ mm}, y2=10+25=35 mmy_2 = 10 + 25 = 35 \text{ mm}
    • A3=15×50=750 mm2A_3 = 15 \times 50 = 750 \text{ mm}^2, x3=70−7.5=62.5 mmx_3 = 70 - 7.5 = 62.5 \text{ mm}, y3=10+25=35 mmy_3 = 10 + 25 = 35 \text{ mm}
    • Total Area A=700+750+750=2200 mm2A = 700 + 750 + 750 = 2200 \text{ mm}^2

    The centroid coordinates are:

    xˉ=A1x1+A2x2+A3x3A=700(35)+750(7.5)+750(62.5)2200=24500+5625+468752200=770002200=35 mm\bar{x} = \frac{A_1 x_1 + A_2 x_2 + A_3 x_3}{A} = \frac{700(35) + 750(7.5) + 750(62.5)}{2200} = \frac{24500 + 5625 + 46875}{2200} = \frac{77000}{2200} = 35 \text{ mm} yˉ=A1y1+A2y2+A3y3A=700(5)+750(35)+750(35)2200=3500+26250+262502200=560002200=28011≈25.45 mm\bar{y} = \frac{A_1 y_1 + A_2 y_2 + A_3 y_3}{A} = \frac{700(5) + 750(35) + 750(35)}{2200} = \frac{3500 + 26250 + 26250}{2200} = \frac{56000}{2200} = \frac{280}{11} \approx 25.45 \text{ mm}
  2. Calculate Moment of Inertia about the x-x axis (IxxI_{xx})

    We use the parallel axis theorem: Ixx=∑(Ixi+Aidyi2)I_{xx} = \sum (I_{xi} + A_i d_{yi}^2), where Ixi=bihi312I_{xi} = \frac{b_i h_i^3}{12}.

    • For R1R_1: Ix1=70×10312=175003 mm4I_{x1} = \frac{70 \times 10^3}{12} = \frac{17500}{3} \text{ mm}^4. dy1=yˉ−y1=28011−5=22511 mmd_{y1} = \bar{y} - y_1 = \frac{280}{11} - 5 = \frac{225}{11} \text{ mm}. A1dy12=700(22511)2=35437500121 mm4A_1 d_{y1}^2 = 700 \left(\frac{225}{11}\right)^2 = \frac{35437500}{121} \text{ mm}^4.
    • For R2R_2: Ix2=15×50312=156250 mm4I_{x2} = \frac{15 \times 50^3}{12} = 156250 \text{ mm}^4. dy2=y2−yˉ=35−28011=10511 mmd_{y2} = y_2 - \bar{y} = 35 - \frac{280}{11} = \frac{105}{11} \text{ mm}. A2dy22=750(10511)2=8268750121 mm4A_2 d_{y2}^2 = 750 \left(\frac{105}{11}\right)^2 = \frac{8268750}{121} \text{ mm}^4.
    • For R3R_3: Ix3=15×50312=156250 mm4I_{x3} = \frac{15 \times 50^3}{12} = 156250 \text{ mm}^4. dy3=y3−yˉ=10511 mmd_{y3} = y_3 - \bar{y} = \frac{105}{11} \text{ mm}. A3dy32=750(10511)2=8268750121 mm4A_3 d_{y3}^2 = 750 \left(\frac{105}{11}\right)^2 = \frac{8268750}{121} \text{ mm}^4.
    Ixx=(175003+35437500121)+(156250+8268750121)+(156250+8268750121)I_{xx} = \left(\frac{17500}{3} + \frac{35437500}{121}\right) + \left(156250 + \frac{8268750}{121}\right) + \left(156250 + \frac{8268750}{121}\right) Ixx=271480000363≈747878.8 mm4I_{xx} = \frac{271480000}{363} \approx 747878.8 \text{ mm}^4

    The Moment of Inertia about the x-x axis is 747878.8 mm4\boxed{\text{747878.8 mm}^4}.

  3. Calculate Moment of Inertia about the y-y axis (IyyI_{yy})

    We use the parallel axis theorem: Iyy=∑(Iyi+Aidxi2)I_{yy} = \sum (I_{yi} + A_i d_{xi}^2), where Iyi=hibi312I_{yi} = \frac{h_i b_i^3}{12}.

    • For R1R_1: Iy1=10×70312=8575003 mm4I_{y1} = \frac{10 \times 70^3}{12} = \frac{857500}{3} \text{ mm}^4. dx1=xˉ−x1=35−35=0 mmd_{x1} = \bar{x} - x_1 = 35 - 35 = 0 \text{ mm}. A1dx12=0A_1 d_{x1}^2 = 0.
    • For R2R_2: Iy2=50×15312=14062.5 mm4I_{y2} = \frac{50 \times 15^3}{12} = 14062.5 \text{ mm}^4. dx2=xˉ−x2=35−7.5=27.5 mmd_{x2} = \bar{x} - x_2 = 35 - 7.5 = 27.5 \text{ mm}. A2dx22=750(27.5)2=567187.5 mm4A_2 d_{x2}^2 = 750 (27.5)^2 = 567187.5 \text{ mm}^4.
    • For R3R_3: Iy3=50×15312=14062.5 mm4I_{y3} = \frac{50 \times 15^3}{12} = 14062.5 \text{ mm}^4. dx3=x3−xˉ=62.5−35=27.5 mmd_{x3} = x_3 - \bar{x} = 62.5 - 35 = 27.5 \text{ mm}. A3dx32=750(27.5)2=567187.5 mm4A_3 d_{x3}^2 = 750 (27.5)^2 = 567187.5 \text{ mm}^4.
    Iyy=(8575003+0)+(14062.5+567187.5)+(14062.5+567187.5)I_{yy} = \left(\frac{857500}{3} + 0\right) + (14062.5 + 567187.5) + (14062.5 + 567187.5) Iyy=8575003+581250+581250=8575003+1162500=43450003≈1448333.3 mm4I_{yy} = \frac{857500}{3} + 581250 + 581250 = \frac{857500}{3} + 1162500 = \frac{4345000}{3} \approx 1448333.3 \text{ mm}^4

    The Moment of Inertia about the y-y axis is 1448333.3 mm4\boxed{\text{1448333.3 mm}^4}.


    Shape 2: I-Beam

    First, we divide the I-beam into three rectangles:

    • R1R_1: Top flange (width b1=40b_1 = 40 mm, height h1=10h_1 = 10 mm)
    • R2R_2: Web (width b2=10b_2 = 10 mm, height h2=30h_2 = 30 mm)
    • R3R_3: Bottom flange (width b3=80b_3 = 80 mm, height h3=10h_3 = 10 mm)
  4. Calculate the Centroid (xˉ,yˉ\bar{x}, \bar{y})

    We set the origin at the bottom-left corner of the bottom flange.

    • A1=40×10=400 mm2A_1 = 40 \times 10 = 400 \text{ mm}^2, x1=40 mmx_1 = 40 \text{ mm}, y1=50−5=45 mmy_1 = 50 - 5 = 45 \text{ mm}
    • A2=10×30=300 mm2A_2 = 10 \times 30 = 300 \text{ mm}^2, x2=40 mmx_2 = 40 \text{ mm}, y2=10+15=25 mmy_2 = 10 + 15 = 25 \text{ mm}
    • A3=80×10=800 mm2A_3 = 80 \times 10 = 800 \text{ mm}^2, x3=40 mmx_3 = 40 \text{ mm}, y3=5 mmy_3 = 5 \text{ mm}
    • Total Area A=400+300+800=1500 mm2A = 400 + 300 + 800 = 1500 \text{ mm}^2

    The centroid coordinates are:

    xˉ=A1x1+A2x2+A3x3A=400(40)+300(40)+800(40)1500=16000+12000+320001500=600001500=40 mm\bar{x} = \frac{A_1 x_1 + A_2 x_2 + A_3 x_3}{A} = \frac{400(40) + 300(40) + 800(40)}{1500} = \frac{16000 + 12000 + 32000}{1500} = \frac{60000}{1500} = 40 \text{ mm} yˉ=A1y1+A2y2+A3y3A=400(45)+300(25)+800(5)1500=18000+7500+40001500=295001500=593≈19.67 mm\bar{y} = \frac{A_1 y_1 + A_2 y_2 + A_3 y_3}{A} = \frac{400(45) + 300(25) + 800(5)}{1500} = \frac{18000 + 7500 + 4000}{1500} = \frac{29500}{1500} = \frac{59}{3} \approx 19.67 \text{ mm}
  5. Calculate Moment of Inertia about the x-x axis (IxxI_{xx})

    We use the parallel axis theorem: Ixx=∑(Ixi+Aidyi2)I_{xx} = \sum (I_{xi} + A_i d_{yi}^2), where Ixi=bihi312I_{xi} = \frac{b_i h_i^3}{12}.

    • For R1R_1: Ix1=40×10312=100003 mm4I_{x1} = \frac{40 \times 10^3}{12} = \frac{10000}{3} \text{ mm}^4. dy1=y1−yˉ=45−593=763 mmd_{y1} = y_1 - \bar{y} = 45 - \frac{59}{3} = \frac{76}{3} \text{ mm}. A1dy12=400(763)2=23104009 mm4A_1 d_{y1}^2 = 400 \left(\frac{76}{3}\right)^2 = \frac{2310400}{9} \text{ mm}^4.
    • For R2R_2: Ix2=10×30312=22500 mm4I_{x2} = \frac{10 \times 30^3}{12} = 22500 \text{ mm}^4. dy2=y2−yˉ=25−593=163 mmd_{y2} = y_2 - \bar{y} = 25 - \frac{59}{3} = \frac{16}{3} \text{ mm}. A2dy22=300(163)2=256003 mm4A_2 d_{y2}^2 = 300 \left(\frac{16}{3}\right)^2 = \frac{25600}{3} \text{ mm}^4.
    • For R3R_3: Ix3=80×10312=200003 mm4I_{x3} = \frac{80 \times 10^3}{12} = \frac{20000}{3} \text{ mm}^4. dy3=yˉ−y3=593−5=443 mmd_{y3} = \bar{y} - y_3 = \frac{59}{3} - 5 = \frac{44}{3} \text{ mm}. A3dy32=800(443)2=15488009 mm4A_3 d_{y3}^2 = 800 \left(\frac{44}{3}\right)^2 = \frac{1548800}{9} \text{ mm}^4.
    Ixx=(100003+23104009)+(22500+256003)+(200003+15488009)I_{xx} = \left(\frac{10000}{3} + \frac{2310400}{9}\right) + \left(22500 + \frac{25600}{3}\right) + \left(\frac{20000}{3} + \frac{1548800}{9}\right) Ixx=42285009=469833.33 mm4I_{xx} = \frac{4228500}{9} = 469833.33 \text{ mm}^4

    The Moment of Inertia about the x-x axis is 469833.3 mm4\boxed{\text{469833.3 mm}^4}.

  6. Calculate Moment of Inertia about the y-y axis (IyyI_{yy})

    We use the parallel axis theorem: Iyy=∑(Iyi+Aidxi2)I_{yy} = \sum (I_{yi} + A_i d_{xi}^2), where Iyi=hibi312I_{yi} = \frac{h_i b_i^3}{12}.
    Since the y-y axis is the axis of symmetry and all component centroids lie on this axis, dxi=0d_{xi} = 0 for all components.

    • For R1R_1: Iy1=10×40312=1600003 mm4I_{y1} = \frac{10 \times 40^3}{12} = \frac{160000}{3} \text{ mm}^4. dx1=0d_{x1} = 0.
    • For R2R_2: Iy2=30×10312=2500 mm4I_{y2} = \frac{30 \times 10^3}{12} = 2500 \text{ mm}^4. dx2=0d_{x2} = 0.
    • For R3R_3: Iy3=10×80312=12800003 mm4I_{y3} = \frac{10 \times 80^3}{12} = \frac{1280000}{3} \text{ mm}^4. dx3=0d_{x3} = 0.
    Iyy=1600003+2500+12800003I_{yy} = \frac{160000}{3} + 2500 + \frac{1280000}{3} Iyy=14400003+2500=480000+2500=482500 mm4I_{yy} = \frac{1440000}{3} + 2500 = 480000 + 2500 = 482500 \text{ mm}^4

    The Moment of Inertia about the y-y axis is 482500 mm4\boxed{\text{482500 mm}^4}.

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