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04-BS-3 · December 2014

Question 3 of 6: Question 3 (paper Question III)

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

National Examination — Statics and Dynamics (04-BS-3), December 2014. 3 hours, closed book (one 8.5"×11" self-prepared note sheet permitted). Candidates were required to complete 2 of the 3 questions in Part A (Statics) and 2 of the 3 questions in Part B (Dynamics); every question in both parts is solved below.

Reference texts: Hibbeler, Engineering Mechanics: Statics; Hibbeler, Engineering Mechanics: Dynamics.

Check — figure readings (Questions 1 and 3): (1) In Figure 1's truss only three members meet at joint D (C–D, D–B, D–E) — there is no separate C–E member, and the truss coordinates are A(0,0), B(4,0), C(1,2), D(3,2.6), E(7,4) m. (2) Figure 3A's axial dimension stack (2+4+2+4+2 = 14 in) does not sum to the labelled overall height of 16 in unless the hub's "2 in." label is read as a half-thickness measured from the shaft centreline (giving a full hub thickness of 4 in, which closes the stack exactly: 2+4+4+4+2 = 16 in). Both readings are disclosed here and used consistently in the solutions below.

Question 3 (paper Question III) (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Part A — Mass moment of inertia and radius of gyration of the flywheel

Given. Axisymmetric steel flywheel, specific weight $\gamma=490\ \text{lb}_f/\text{ft}^3$. Five hollow-cylinder segments stacked along the axis of rotation (see the callout above for the 16 in reconciliation):

Flywheel segments (about the axis of rotation)
SegmentOuter R (in)Inner r (in)Axial thickness (in)
Rim (top)422
Web plate (top, "1 in thick solid plate")421
Hub324
Web plate (bottom)421
Rim (bottom)422

Find. $I_m$ and $k=\sqrt{I_m/M}$ about the axis of rotation.

axis of rotationR=4 inR=3 inr=2 in bore16 in overallHub 4in × (R3,r2); web 1in solid × (R4,r2); rim 2in × (R4,r2)
Figure 3A — flywheel cross-section (axis of rotation horizontal, radii shown to scale).

Approach. Treat every segment as a hollow cylinder about the same central axis; compute each segment's weight from $\gamma\times$ volume, convert to mass, apply $I_m=\tfrac12 m(R^2+r^2)$, and sum. Work in feet so $\gamma$ ($\text{lb}_f/\text{ft}^3$) and $g=32.2\ \text{ft/s}^2$ are dimensionally consistent, giving $I_m$ in $\text{slug}\cdot\text{ft}^2$.

  1. Mass of each segment. $V=\pi(R^2-r^2)t$, $W=\gamma V$, $m=W/g$. Converting each $R,r,t$ to feet ($\div 12$):
    Segment$V$ (ft³)$m$ (slug)
    Rim ×20.043630.6640 each
    Web ×20.021820.3320 each
    Hub0.036360.5533
    Total mass $M = 2(0.6640)+2(0.3320)+0.5533 = 2.545\ \text{slug}$ (weight $\approx 81.96\ \text{lb}_f$).
  2. Moment of inertia of each segment about the axis ($I_m=\tfrac12 m(R^2+r^2)$, R,r in ft): $$I_{\text{rim}} = \tfrac12(0.6640)\!\left[\left(\tfrac{4}{12}\right)^2+\left(\tfrac{2}{12}\right)^2\right] = 0.04611\ \text{slug}\cdot\text{ft}^2 \ \text{(each; ×2 rims)}$$ $$I_{\text{web}} = \tfrac12(0.3320)\!\left[\left(\tfrac{4}{12}\right)^2+\left(\tfrac{2}{12}\right)^2\right] = 0.02305\ \text{slug}\cdot\text{ft}^2 \ \text{(each; ×2 webs)}$$ $$I_{\text{hub}} = \tfrac12(0.5533)\!\left[\left(\tfrac{3}{12}\right)^2+\left(\tfrac{2}{12}\right)^2\right] = 0.02498\ \text{slug}\cdot\text{ft}^2$$
  3. Sum. $$I_m = 2(0.04611)+2(0.02305)+0.02498 = 0.1633\ \text{slug}\cdot\text{ft}^2$$ $$\boxed{I_m = 0.163\ \text{slug}\cdot\text{ft}^2 = 1.958\ \text{lb}_f\cdot\text{in}\cdot\text{s}^2}$$
  4. Radius of gyration. $$k = \sqrt{\frac{I_m}{M}} = \sqrt{\frac{0.1633}{2.545}} = 0.2533\ \text{ft}$$ $$\boxed{k = 3.04\ \text{in}}$$
Flywheel mass properties
QuantityValue
Total weight, $W$82.0 $\text{lb}_f$
Total mass, $M$2.545 slug
Mass moment of inertia, $I_m$0.163 slug·ft² (1.96 $\text{lb}_f\cdot\text{in}\cdot\text{s}^2$)
Radius of gyration, $k$3.04 in (0.253 ft)
Check: the hub's full axial thickness (4 in, treated as symmetric about the shaft centreline) and the web's radial span (bore to rim inner radius, R=4 in, r=2 in) are read from the printed figure per the reconciliation callout above; the arithmetic method and formula application are exact given these dimensions.

Part B — Centroid of the area under $y=b(1-kx^3)$ by direct integration

Given. Plane area in the first quadrant bounded by the $x$-axis, the $y$-axis, and the curve $y=b(1-kx^3)$, with $y$-intercept $b$ (at $x=0$) and $x$-intercept $a$ (at $x=a$).

Find. The centroid $(\bar x,\bar y)$ in terms of $a$ and $b$, by direct integration.

xyabC (2a/5, 3b/7)y = b(1 − x³/a³)
Figure 3B — area under $y=b(1-x^3/a^3)$ with its centroid.

Approach. Since the $x$-intercept is $a$, the constant $k=1/a^3$, so $y=b(1-x^3/a^3)$. Use single-integration (vertical strip) formulas $A=\int y\,dx$, $\bar x A=\int xy\,dx$, $\bar y A = \int \tfrac{y^2}{2}\,dx$.

  1. Area. $$A = \int_0^a b\!\left(1-\frac{x^3}{a^3}\right)dx = b\left[x-\frac{x^4}{4a^3}\right]_0^a = b\left(a-\frac{a}{4}\right) = \frac{3ab}{4}$$
  2. First moment about the $y$-axis, for $\bar x$. $$\int_0^a x\,y\,dx = b\int_0^a\!\left(x-\frac{x^4}{a^3}\right)dx = b\left(\frac{a^2}{2}-\frac{a^2}{5}\right) = \frac{3a^2b}{10}$$ $$\bar x = \frac{3a^2b/10}{3ab/4} = \frac{4a}{10} = \boxed{\frac{2a}{5}}$$
  3. First moment about the $x$-axis, for $\bar y$. $$\int_0^a \frac{y^2}{2}\,dx = \frac{b^2}{2}\int_0^a\!\left(1-\frac{2x^3}{a^3}+\frac{x^6}{a^6}\right)dx = \frac{b^2}{2}\left(a-\frac{a}{2}+\frac{a}{7}\right) = \frac{9ab^2}{28}$$ $$\bar y = \frac{9ab^2/28}{3ab/4} = \frac{9b}{28}\cdot\frac{4}{3} = \boxed{\frac{3b}{7}}$$
Centroid of the area under $y=b(1-x^3/a^3)$
QuantityResult
Area, $A$$3ab/4$
$\bar x$$2a/5 = 0.400a$
$\bar y$$3b/7 = 0.4286b$