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Statics (Extended)

Statics (Extended Treatment)

This document covers moments, equilibrium conditions, centres of mass, ladder problems, and frameworks with a rigorous, proof-based approach.

info

Statics problems require careful consideration of every force and every moment. A systematic approach -- drawing the diagram, listing forces, choosing a pivot -- is more reliable than intuition.


1. Moments

1.1 Definition

The moment of a force F\mathbf{F} about a point OO is:

MO=F×dM_O = F \times d

where dd is the perpendicular distance from the line of action of the force to the point OO.

The SI unit of moment is the newton-metre (Nm\mathrm{Nm}).

Sign convention: By convention, anticlockwise moments are positive and clockwise moments are negative.

1.2 Moment of a force at an angle

If a force FF acts at angle θ\theta to the line joining the point of application to the pivot, the moment is M=FdsinθM = Fd\sin\theta, where dd is the distance from the pivot to the point of application.

Proof. Resolve the force into components parallel and perpendicular to the line from the pivot to the point of application. The parallel component passes through the pivot and produces zero moment. The perpendicular component is FsinθF\sin\theta, and its moment is Fsinθ×dF\sin\theta \times d. \blacksquare

1.3 Worked example: beam on two supports

Problem. A uniform beam ABAB of mass 20  kg20\;\mathrm{kg} and length 4  m4\;\mathrm{m} rests horizontally on supports at AA and at a point CC, 1  m1\;\mathrm{m} from BB. A load of 50  N50\;\mathrm{N} is hung from the beam at a point 0.5  m0.5\;\mathrm{m} from AA. Find the reactions at AA and CC.

Taking moments about AA (anticlockwise positive):

Weight of beam: 20g  N20g\;\mathrm{N} acting at the midpoint, 2  m2\;\mathrm{m} from AA.

RC×320g×250×0.5=0R_C \times 3 - 20g \times 2 - 50 \times 0.5 = 0

RC=40g+253=392+253=4173=139  NR_C = \frac{40g + 25}{3} = \frac{392 + 25}{3} = \frac{417}{3} = 139\;\mathrm{N}

Resolving vertically: RA+RC=20g+50R_A + R_C = 20g + 50

RA=20g+50139=196+50139=107  NR_A = 20g + 50 - 139 = 196 + 50 - 139 = 107\;\mathrm{N}

warning

Common Pitfall When taking moments, always measure the perpendicular distance from the line of action of the force to the pivot point, not just the distance along the beam.


2. Equilibrium of a Rigid Body

2.1 Conditions for equilibrium

A rigid body is in equilibrium if and only if:

  1. The resultant force is zero: F=0\sum \mathbf{F} = \mathbf{0}

  2. The resultant moment about any point is zero: MO=0for any point O\sum M_O = 0 \quad \mathrm{for\ any\ point}\ O

Theorem. If the resultant force on a body is zero and the resultant moment about one point is zero, then the resultant moment about every point is zero.

Proof. Suppose F=0\sum \mathbf{F} = \mathbf{0} and MA=0\sum M_A = 0. For any other point BB:

MB=MA+rBA×F=0+rBA×0=0M_B = M_A + \mathbf{r}_{BA} \times \sum \mathbf{F} = 0 + \mathbf{r}_{BA} \times \mathbf{0} = 0

where rBA\mathbf{r}_{BA} is the position vector from BB to AA. \blacksquare

This theorem means we only need to take moments about one point, but we can choose any point to simplify the calculation.

2.2 Resolving forces in two dimensions

For equilibrium in 2D, we resolve horizontally and vertically:

Fx=0,Fy=0,M=0\sum F_x = 0, \qquad \sum F_y = 0, \qquad \sum M = 0

This gives three equations, which can determine up to three unknowns.

2.3 Worked example: non-uniform beam

Problem. A non-uniform beam ABAB of length 6  m6\;\mathrm{m} and mass 30  kg30\;\mathrm{kg} rests on supports at AA and BB. When a load of 200  N200\;\mathrm{N} is placed at a point 2  m2\;\mathrm{m} from AA, the reaction at AA is 350  N350\;\mathrm{N}. Find the position of the centre of mass of the beam.

Let the centre of mass be at distance xx from AA. Taking moments about BB (anticlockwise positive):

The beam's weight 30g30g acts downward at distance xx from AA, which is (6x)(6 - x) from BB. The 200  N200\;\mathrm{N} load acts at distance 4  m4\;\mathrm{m} from BB. The reaction at AA (350  N350\;\mathrm{N}) acts at distance 6  m6\;\mathrm{m} from BB.

350×6+200×430g(6x)=0350 \times 6 + 200 \times 4 - 30g(6 - x) = 0

2100+800294(6x)=02100 + 800 - 294(6 - x) = 0

2900=1764294x2900 = 1764 - 294x

294x=17642900=1136294x = 1764 - 2900 = -1136

Wait -- this gives a negative result, which suggests an error in sign convention. Let me reconsider.

Taking moments about BB with anticlockwise positive: forces pushing the beam to rotate anticlockwise about BB contribute positively.

RA=350  NR_A = 350\;\mathrm{N} acts upward at distance 6  m6\;\mathrm{m} from BB: moment =+350×6=2100= +350 \times 6 = 2100.

200  N200\;\mathrm{N} acts downward at distance 4  m4\;\mathrm{m} from BB: moment =200×4=800= -200 \times 4 = -800.

30g  N30g\;\mathrm{N} acts downward at distance (6x)(6-x) from BB: moment =30g(6x)= -30g(6-x).

210080030g(6x)=02100 - 800 - 30g(6-x) = 0

1300=294(6x)=1764294x1300 = 294(6-x) = 1764 - 294x

294x=464    x=4642941.58  m294x = 464 \implies x = \frac{464}{294} \approx 1.58\;\mathrm{m}

The centre of mass is approximately 1.58  m1.58\;\mathrm{m} from AA.


3. Centres of Mass

3.1 Centre of mass of a system of particles

For particles of masses m1,m2,,mnm_1, m_2, \ldots, m_n at positions (x1,y1),(x2,y2),,(xn,yn)(x_1, y_1), (x_2, y_2), \ldots, (x_n, y_n):

xˉ=LBmixiRB◆◆LBmiRB,yˉ=LBmiyiRB◆◆LBmiRB\bar{x} = \frac◆LB◆\sum m_i x_i◆RB◆◆LB◆\sum m_i◆RB◆, \qquad \bar{y} = \frac◆LB◆\sum m_i y_i◆RB◆◆LB◆\sum m_i◆RB◆

3.2 Centre of mass of uniform laminas

Uniform rod: Midpoint.

Uniform rectangular lamina: Intersection of the diagonals.

Uniform triangular lamina: At the intersection of the medians, which is at a distance 23\dfrac{2}{3} of the median length from each vertex.

Proof for a triangle. Place the triangle with vertices at (0,0)(0,0), (a,0)(a,0), and (0,b)(0,b). A strip parallel to the base at height yy has width a ⁣(1yb)a\!\left(1 - \dfrac{y}{b}\right) and mass proportional to this width.

yˉ=LB0bya ⁣(1yb)dyRB◆◆LB0ba ⁣(1yb)dyRB=LB[y22y33b]0bRB◆◆LB[yy22b]0bRB=LBb22b23RB◆◆LBbb2RB=LBb26RB◆◆LBb2RB=b3\bar{y} = \frac◆LB◆\int_0^b y \cdot a\!\left(1 - \frac{y}{b}\right)dy◆RB◆◆LB◆\int_0^b a\!\left(1 - \frac{y}{b}\right)dy◆RB◆ = \frac◆LB◆\left[\frac{y^2}{2} - \frac{y^3}{3b}\right]_0^b◆RB◆◆LB◆\left[y - \frac{y^2}{2b}\right]_0^b◆RB◆ = \frac◆LB◆\frac{b^2}{2} - \frac{b^2}{3}◆RB◆◆LB◆b - \frac{b}{2}◆RB◆ = \frac◆LB◆\frac{b^2}{6}◆RB◆◆LB◆\frac{b}{2}◆RB◆ = \frac{b}{3}

The centre of mass is at height b3\dfrac{b}{3}, which is 13\dfrac{1}{3} of the way from the base and 23\dfrac{2}{3} from the apex. \blacksquare

3.3 Composite bodies

For a body composed of several parts with known centres of mass, the overall centre of mass is found by treating each part as a particle at its own centre of mass.

3.4 Worked example: composite lamina

Problem. A uniform lamina consists of a rectangle ABCDABCD with AB=8  cmAB = 8\;\mathrm{cm}, BC=6  cmBC = 6\;\mathrm{cm}, with a semicircle of diameter 8  cm8\;\mathrm{cm} removed from the top edge ADAD. Find the centre of mass of the remaining lamina.

Rectangle: area =48  cm2= 48\;\mathrm{cm}^2, centre at (4,3)(4, 3).

Semicircle: radius =4  cm= 4\;\mathrm{cm}, area =12π(16)=8π  cm2= \dfrac{1}{2}\pi(16) = 8\pi\;\mathrm{cm}^2. Centre of mass of the semicircle is at distance LB4rRB◆◆LB3πRB=LB16RB◆◆LB3πRB\dfrac◆LB◆4r◆RB◆◆LB◆3\pi◆RB◆ = \dfrac◆LB◆16◆RB◆◆LB◆3\pi◆RB◆ from the diameter, i.e. at (4,6LB16RB◆◆LB3πRB)(4, 6 - \dfrac◆LB◆16◆RB◆◆LB◆3\pi◆RB◆).

Treating the removed semicircle as a negative mass:

xˉ=LB48×48π×4RB◆◆LB488πRB=LB4(488π)RB◆◆LB488πRB=4  cm\bar{x} = \frac◆LB◆48 \times 4 - 8\pi \times 4◆RB◆◆LB◆48 - 8\pi◆RB◆ = \frac◆LB◆4(48 - 8\pi)◆RB◆◆LB◆48 - 8\pi◆RB◆ = 4\;\mathrm{cm}

This is expected by symmetry.

yˉ=LB48×38π ⁣(6LB16RB◆◆LB3πRB)RB◆◆LB488πRB=LB14448π+1283RB◆◆LB488πRB\bar{y} = \frac◆LB◆48 \times 3 - 8\pi\!\left(6 - \frac◆LB◆16◆RB◆◆LB◆3\pi◆RB◆\right)◆RB◆◆LB◆48 - 8\pi◆RB◆ = \frac◆LB◆144 - 48\pi + \frac{128}{3}◆RB◆◆LB◆48 - 8\pi◆RB◆

yˉ=144+42.67150.804825.13=35.8722.871.57  cm\bar{y} = \frac{144 + 42.67 - 150.80}{48 - 25.13} = \frac{35.87}{22.87} \approx 1.57\;\mathrm{cm}

warning

Common Pitfall When a shape has a hole or a section removed, use the negative mass method: treat the removed section as having negative area. The formula remains the same but with negative contributions from the removed part.


4. Ladder Problems

4.1 General approach

Ladder problems involve a uniform ladder leaning against a rough vertical wall and resting on a rough horizontal ground. The key forces are:

  • Weight WW of the ladder, acting at the centre.
  • Normal reaction RgR_g from the ground (vertical).
  • Friction FgF_g from the ground (horizontal).
  • Normal reaction RwR_w from the wall (horizontal).
  • Friction FwF_w from the wall (vertical).

4.2 Worked example: ladder on rough ground and smooth wall

Problem. A uniform ladder of length 5  m5\;\mathrm{m} and mass 20  kg20\;\mathrm{kg} rests with its foot on rough horizontal ground and its top against a smooth vertical wall. The ladder makes an angle of 6565^\circ with the horizontal. The coefficient of friction between the ladder and the ground is 0.40.4. Will the ladder slip?

Resolving horizontally: Fg=RwF_g = R_w.

Resolving vertically: Rg=20g=196  NR_g = 20g = 196\;\mathrm{N}.

Taking moments about the foot of the ladder (anticlockwise positive):

Rw×5sin6520g×2.5cos65=0R_w \times 5\sin 65^\circ - 20g \times 2.5\cos 65^\circ = 0

Rw=LB20g×2.5cos65RB◆◆LB5sin65RB=LB49cos65RB◆◆LBsin65RB=49cot65R_w = \frac◆LB◆20g \times 2.5\cos 65^\circ◆RB◆◆LB◆5\sin 65^\circ◆RB◆ = \frac◆LB◆49\cos 65^\circ◆RB◆◆LB◆\sin 65^\circ◆RB◆ = 49\cot 65^\circ

Rw=49×0.4663=22.85  NR_w = 49 \times 0.4663 = 22.85\;\mathrm{N}

Fg=Rw=22.85  NF_g = R_w = 22.85\;\mathrm{N}

Maximum available friction: Fmax=μRg=0.4×196=78.4  NF_{\max} = \mu R_g = 0.4 \times 196 = 78.4\;\mathrm{N}.

Since Fg=22.85<78.4=FmaxF_g = 22.85 \lt 78.4 = F_{\max}, the ladder does not slip.

4.3 Finding the minimum angle

Problem. For the same ladder, find the minimum angle with the horizontal for equilibrium.

At the limiting position, Fg=μRgF_g = \mu R_g:

Rw=Fg=μRg=0.4×196=78.4  NR_w = F_g = \mu R_g = 0.4 \times 196 = 78.4\;\mathrm{N}

Taking moments about the foot:

Rw×5sinα=20g×2.5cosαR_w \times 5\sin\alpha = 20g \times 2.5\cos\alpha

78.4×5sinα=490cosα78.4 \times 5\sin\alpha = 490\cos\alpha

tanα=490392=1.25\tan\alpha = \frac{490}{392} = 1.25

α=arctan(1.25)51.3\alpha = \arctan(1.25) \approx 51.3^\circ

The minimum angle is approximately 51.351.3^\circ.

warning

warning In ladder problems, always take moments about the foot of the ladder (or the point where two unknown forces act) to eliminate as many unknowns as possible from the moment equation.


5. Frameworks

5.1 Method of joints

A framework (or truss) is a structure made of light rods joined at points called joints (or nodes). To analyse a framework:

  1. Find the external reactions (support forces) using equilibrium of the whole structure.
  2. Analyse each joint in turn, resolving forces in two perpendicular directions.
  3. Determine whether each rod is in tension (pulling) or compression (pushing).

Assumptions:

  • All rods are light (weightless).
  • All joints are smooth pin joints.
  • All forces act along the rods (no bending).

5.2 Worked example: simple truss

Problem. A framework consists of six light rods forming a equilateral triangle ABCABC (side 2  m2\;\mathrm{m}) with midpoints DD, EE, FF on ABAB, BCBC, CACA respectively, connected to the opposite vertices. A vertical load of 100  N100\;\mathrm{N} acts at AA. The framework is supported at BB and CC on smooth horizontal surfaces. Find the forces in all rods.

By symmetry, the vertical reactions at BB and CC are equal:

RB=RC=50  NR_B = R_C = 50\;\mathrm{N}

Joint AA: Vertical equilibrium: TADsin60+TAEsin60=100T_{AD}\sin 60^\circ + T_{AE}\sin 60^\circ = 100.

By symmetry, TAD=TAET_{AD} = T_{AE}:

2TADsin60=100    TAD=LB100RB◆◆LB2sin60RB=LB100RB◆◆LB3RB57.7  N2T_{AD}\sin 60^\circ = 100 \implies T_{AD} = \frac◆LB◆100◆RB◆◆LB◆2\sin 60^\circ◆RB◆ = \frac◆LB◆100◆RB◆◆LB◆\sqrt{3}◆RB◆ \approx 57.7\;\mathrm{N}

Both ADAD and AEAE are in tension (pulling away from AA).

Joint BB: Horizontal: TBD=RBcot60=50/328.9  NT_{BD} = R_B\cot 60^\circ = 50/\sqrt{3} \approx 28.9\;\mathrm{N} (tension).

Vertical: TBF=RB=50  NT_{BF} = R_B = 50\;\mathrm{N} (compression, pushing into BB).

This analysis continues joint by joint until all rod forces are determined.

5.3 Method of sections

For large frameworks, the method of sections is often more efficient. An imaginary cut is made through the framework, and equilibrium of one of the resulting sections is analysed.


6. Practice Problems

Problem 1

A uniform beam ABAB of length 5  m5\;\mathrm{m} and weight 200  N200\;\mathrm{N} is hinged at AA and supported by a wire attached at BB, making an angle of 3030^\circ with the beam. Find the tension in the wire and the reaction at the hinge.

Solution

Taking moments about AA:

T×5sin30200×2.5=0T \times 5\sin 30^\circ - 200 \times 2.5 = 0

T=5002.5=200  NT = \frac{500}{2.5} = 200\;\mathrm{N}

Resolving at AA: horizontal reaction H=Tcos30=200cos30=173.2  NH = T\cos 30^\circ = 200\cos 30^\circ = 173.2\;\mathrm{N}.

Vertical reaction V=200Tsin30=200100=100  NV = 200 - T\sin 30^\circ = 200 - 100 = 100\;\mathrm{N}.

Problem 2

A uniform lamina is formed from a square of side 10  cm10\;\mathrm{cm} with a right-angled triangle of base 10  cm10\;\mathrm{cm} and height 6  cm6\;\mathrm{cm} attached to one side. Find the centre of mass of the composite lamina.

Solution

Square: area =100= 100, centre at (5,5)(5, 5). Triangle: area =30= 30, centre at (103,3)\left(\dfrac{10}{3}, 3\right) (one-third from the base).

xˉ=LB100×5+30×103RB◆◆LB130RB=500+100130=6001304.62  cm\bar{x} = \frac◆LB◆100 \times 5 + 30 \times \frac{10}{3}◆RB◆◆LB◆130◆RB◆ = \frac{500 + 100}{130} = \frac{600}{130} \approx 4.62\;\mathrm{cm}

yˉ=LB100×5+30×3RB◆◆LB130RB=500+90130=5901304.54  cm\bar{y} = \frac◆LB◆100 \times 5 + 30 \times 3◆RB◆◆LB◆130◆RB◆ = \frac{500 + 90}{130} = \frac{590}{130} \approx 4.54\;\mathrm{cm}

Problem 3

A uniform ladder of length 8  m8\;\mathrm{m} and mass 25  kg25\;\mathrm{kg} rests against a rough vertical wall (coefficient of friction 0.30.3) on rough horizontal ground (coefficient of friction 0.40.4). The ladder makes an angle of 5555^\circ with the horizontal. A man of mass 75  kg75\;\mathrm{kg} stands on the ladder at a point 5  m5\;\mathrm{m} from the foot. Determine whether the ladder is in equilibrium.

Solution

Resolving vertically: Rg=(25+75)g=980  NR_g = (25 + 75)g = 980\;\mathrm{N}.

Resolving horizontally: Fg=RwF_g = R_w.

Taking moments about the foot:

Rw×8sin5525g×4cos5575g×5cos55=0R_w \times 8\sin 55^\circ - 25g \times 4\cos 55^\circ - 75g \times 5\cos 55^\circ = 0

Rw=LBg(100+375)cos55RB◆◆LB8sin55RB=LB475gcot55RB◆◆LB8RB=LB475×9.8×0.7002RB◆◆LB8RBR_w = \frac◆LB◆g(100 + 375)\cos 55^\circ◆RB◆◆LB◆8\sin 55^\circ◆RB◆ = \frac◆LB◆475g\cot 55^\circ◆RB◆◆LB◆8◆RB◆ = \frac◆LB◆475 \times 9.8 \times 0.7002◆RB◆◆LB◆8◆RB◆

Rw407.5  NR_w \approx 407.5\;\mathrm{N}

So Fg=407.5  NF_g = 407.5\;\mathrm{N}. Available friction at ground: 0.4×980=392  N0.4 \times 980 = 392\;\mathrm{N}.

Available friction at wall: Fw0.3Rw=0.3×407.5=122.3  NF_w \leq 0.3 R_w = 0.3 \times 407.5 = 122.3\;\mathrm{N}.

For vertical equilibrium at the wall: Fw+25g+75g=RgF_w + 25g + 75g = R_g, which gives Fw=0F_w = 0 by our equation. But we should check: resolving vertically for the whole system gives Rg=980  NR_g = 980\;\mathrm{N} and the wall friction FwF_w acts upward.

Taking moments about the foot again with FwF_w included:

Rw×8sin55+Fw×8cos55=475gcos55+25g×4cos55R_w \times 8\sin 55^\circ + F_w \times 8\cos 55^\circ = 475g\cos 55^\circ + 25g \times 4\cos 55^\circ

This gives Fw=0F_w = 0 by the vertical resolution. Since Fg=407.5>392F_g = 407.5 \gt 392, the ladder would slip at the ground.

Problem 4

A uniform rod ABAB of length 3  m3\;\mathrm{m} and weight 80  N80\;\mathrm{N} is freely hinged at AA to a vertical wall. The rod is held horizontal by a string attached to BB and to a point CC on the wall 2  m2\;\mathrm{m} above AA. A load of 120  N120\;\mathrm{N} is hung from BB. Find the tension in the string.

Solution

The string BCBC has length 9+4=13  m\sqrt{9 + 4} = \sqrt{13}\;\mathrm{m}.

sinθ=LB2RB◆◆LB13RB\sin\theta = \dfrac◆LB◆2◆RB◆◆LB◆\sqrt{13}◆RB◆ where θ\theta is the angle between the string and the rod.

Taking moments about AA:

T×3×LB2RB◆◆LB13RB80×1.5120×3=0T \times 3 \times \dfrac◆LB◆2◆RB◆◆LB◆\sqrt{13}◆RB◆ - 80 \times 1.5 - 120 \times 3 = 0

T=LB120+360RB◆◆LB6/13RB=LB48013RB◆◆LB6RB=8013288.4  NT = \frac◆LB◆120 + 360◆RB◆◆LB◆6/\sqrt{13}◆RB◆ = \frac◆LB◆480\sqrt{13}◆RB◆◆LB◆6◆RB◆ = 80\sqrt{13} \approx 288.4\;\mathrm{N}