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Section A: Long Answer Questions

Attempt all questions.

5 questions
1long10 marks

Four coplanar forces act on a rigid square plate ABCDABCD of side 2m2\,\text{m} (corners labelled anticlockwise, with AA at the origin, BB at (2,0)(2,0), CC at (2,2)(2,2) and DD at (0,2)(0,2), distances in metres). The forces are:

  • F1=100NF_1 = 100\,\text{N} acting along ABAB (from AA towards BB),
  • F2=80NF_2 = 80\,\text{N} acting along BCBC (from BB towards CC),
  • F3=60NF_3 = 60\,\text{N} acting along CACA (from CC towards AA),
  • F4=120NF_4 = 120\,\text{N} acting along DADA (from DD towards AA).

Determine the magnitude and direction of the resultant of this force system, and locate its line of action by finding its intercept on the xx-axis.

Step 1 — Resolve each force into components.

Unit vectors along each line of action (tip minus tail, normalised):

  • ABAB: from A(0,0)A(0,0) to B(2,0)B(2,0) → direction (1,0)(1,0). So F1=(100,0)NF_1=(100,\,0)\,\text{N}.
  • BCBC: from B(2,0)B(2,0) to C(2,2)C(2,2) → direction (0,1)(0,1). So F2=(0,80)NF_2=(0,\,80)\,\text{N}.
  • CACA: from C(2,2)C(2,2) to A(0,0)A(0,0) → vector (2,2)(-2,-2), length 222\sqrt2, unit (12,12)(-\tfrac{1}{\sqrt2},-\tfrac{1}{\sqrt2}). So F3=(60/2,60/2)=(42.43,42.43)NF_3=(-60/\sqrt2,\,-60/\sqrt2)=(-42.43,\,-42.43)\,\text{N}.
  • DADA: from D(0,2)D(0,2) to A(0,0)A(0,0) → direction (0,1)(0,-1). So F4=(0,120)NF_4=(0,\,-120)\,\text{N}.

Step 2 — Sum the components.

Rx=100+042.43+0=57.57NR_x=100+0-42.43+0=57.57\,\text{N} Ry=0+8042.43120=82.43NR_y=0+80-42.43-120=-82.43\,\text{N}

Step 3 — Magnitude and direction.

R=57.572+(82.43)2=3314.3+6794.7=10109.0=100.5NR=\sqrt{57.57^2+(-82.43)^2}=\sqrt{3314.3+6794.7}=\sqrt{10109.0}=100.5\,\text{N} θ=tan1 ⁣(RyRx)=tan1 ⁣(82.4357.57)=55.07\theta=\tan^{-1}\!\left(\frac{|R_y|}{|R_x|}\right)=\tan^{-1}\!\left(\frac{82.43}{57.57}\right)=55.07^\circ

Since Rx>0R_x>0 and Ry<0R_y<0, the resultant lies in the fourth quadrant: R=100.5NR=100.5\,\text{N} directed 55.155.1^\circ below the positive xx-axis.

Step 4 — Moment about origin AA (use M=xFyyFxM=x F_y - y F_x at each force's point of application).

Take a convenient point on each line of action:

  • F1F_1 at A(0,0)A(0,0): M=0M=0.
  • F2F_2 at B(2,0)B(2,0): M=2(80)0(0)=160N\cdotpmM=2(80)-0(0)=160\,\text{N·m}.
  • F3F_3 at C(2,2)C(2,2): M=2(42.43)2(42.43)=0N\cdotpmM=2(-42.43)-2(-42.43)=0\,\text{N·m} (line passes through AA).
  • F4F_4 at D(0,2)D(0,2): M=0(120)2(0)=0N\cdotpmM=0(-120)-2(0)=0\,\text{N·m}.

Net moment about AA: MA=160N\cdotpmM_A=160\,\text{N·m} (anticlockwise positive).

Step 5 — Locate line of action (x-intercept).

The resultant must produce the same moment about AA. For the resultant crossing the xx-axis at (x,0)(x,0), only RyR_y contributes a moment about AA:

MA=xRy    160=x(82.43)    x=1.94m.M_A = x\,R_y \;\Rightarrow\; 160 = x(-82.43) \;\Rightarrow\; x = -1.94\,\text{m}.

The resultant of magnitude 100.5N100.5\,\text{N} acts at 55.155.1^\circ below the +x+x-axis and crosses the xx-axis at x=1.94mx=-1.94\,\text{m}.

force-systemsresultantmoment
2long10 marks

A simply supported pin-jointed plane truss spans 12m12\,\text{m}. The bottom chord has joints AA, CC, EE (and the support) spaced at 4m4\,\text{m}: A(0,0)A(0,0), C(4,0)C(4,0), E(8,0)E(8,0), G(12,0)G(12,0). The top chord joints are B(4,3)B(4,3), D(8,3)D(8,3). Members form the pattern: ABAB, BCBC, BDBD, CDCD, DEDE, DGDG on the upper portion together with bottom chord ACAC, CECE, EGEG, plus diagonal/vertical members ABAB, CDCD, EGEG as drawn. The truss is supported by a pin at AA and a roller at GG. Vertical downward loads of 20kN20\,\text{kN} act at BB and 30kN30\,\text{kN} at DD.

For simplicity treat the truss as the two-panel configuration with joints A(0,0)A(0,0), C(6,0)C(6,0), G(12,0)G(12,0) on the bottom chord and apex joints B(3,4)B(3,4) and D(9,4)D(9,4) on top, members AB,BC,BD,DC,DGAB, BC, BD, DC, DG and bottom chord AC,CGAC, CG. Loads: 20kN20\,\text{kN} down at BB, 30kN30\,\text{kN} down at DD.

(a) Find the support reactions. (b) Using the method of joints, determine the forces in members ABAB, ACAC and BCBC, stating tension or compression.

We analyse the simplified two-panel truss: A(0,0)A(0,0) pin, G(12,0)G(12,0) roller; C(6,0)C(6,0) bottom; apexes B(3,4)B(3,4), D(9,4)D(9,4). Loads 20kN20\,\text{kN}\downarrow at BB, 30kN30\,\text{kN}\downarrow at DD.

Part (a) — Support reactions.

Total downward load =20+30=50kN=20+30=50\,\text{kN}. Pin at AA gives Ax,AyA_x,A_y; roller at GG gives GyG_y.

Fx=0\sum F_x=0: no horizontal loads, so Ax=0A_x=0.

MA=0\sum M_A=0 (anticlockwise +): Gy(12)20(3)30(9)=0G_y(12) - 20(3) - 30(9)=0

12Gy=60+270=330Gy=27.5kN  ()12G_y = 60+270 = 330 \Rightarrow G_y = 27.5\,\text{kN}\;(\uparrow)

Fy=0\sum F_y=0: Ay+Gy50=0Ay=5027.5=22.5kN  ()A_y + G_y - 50 = 0 \Rightarrow A_y = 50 - 27.5 = 22.5\,\text{kN}\;(\uparrow).

Reactions: Ax=0A_x=0, Ay=22.5kNA_y=22.5\,\text{kN}\uparrow, Gy=27.5kNG_y=27.5\,\text{kN}\uparrow.

Part (b) — Method of joints.

Member ABAB direction: from A(0,0)A(0,0) to B(3,4)B(3,4), length =32+42=5m=\sqrt{3^2+4^2}=5\,\text{m}; direction cosines cosα=3/5=0.6\cos\alpha=3/5=0.6, sinα=4/5=0.8\sin\alpha=4/5=0.8.

Joint AA (members ABAB and ACAC; reaction Ay=22.5kNA_y=22.5\,\text{kN}\uparrow, Ax=0A_x=0). Assume members in tension (pulling away from joint).

Fy=0\sum F_y=0: Ay+FABsinα=0A_y + F_{AB}\sin\alpha = 0

22.5+FAB(0.8)=0FAB=28.125kN22.5 + F_{AB}(0.8)=0 \Rightarrow F_{AB} = -28.125\,\text{kN}

Negative ⇒ FAB=28.13kN (Compression)F_{AB}=28.13\,\text{kN (Compression)}.

Fx=0\sum F_x=0: FAC+FABcosα=0F_{AC} + F_{AB}\cos\alpha = 0

FAC=FAB(0.6)=(28.125)(0.6)=16.875kNF_{AC} = -F_{AB}(0.6) = -(-28.125)(0.6)=16.875\,\text{kN}

Positive ⇒ FAC=16.88kN (Tension)F_{AC}=16.88\,\text{kN (Tension)}.

Joint BB (members BABA, BCBC, BDBD; load 20kN20\,\text{kN}\downarrow). BABA runs from B(3,4)B(3,4) to A(0,0)A(0,0): direction (0.6,0.8)(-0.6,-0.8). BDBD is horizontal from B(3,4)B(3,4) to D(9,4)D(9,4): direction (1,0)(1,0). BCBC from B(3,4)B(3,4) to C(6,0)C(6,0): vector (3,4)(3,-4), length 55, direction (0.6,0.8)(0.6,-0.8).

Known FBA=FAB=28.125kNF_{BA}=F_{AB}=-28.125\,\text{kN} (compression). Force on joint BB from member BABA (tension convention, pulling toward AA): FBA(0.6,0.8)=(28.125)(0.6,0.8)=(16.875,22.5)kNF_{BA}\,(-0.6,-0.8) = (-28.125)(-0.6,-0.8)=(16.875,\,22.5)\,\text{kN}.

Fy=0\sum F_y=0 at BB: 22.5+FBC(0.8)20=022.5 + F_{BC}(-0.8) - 20 = 0

2.50.8FBC=0FBC=3.125kN2.5 - 0.8 F_{BC}=0 \Rightarrow F_{BC}=3.125\,\text{kN}

Positive ⇒ FBC=3.13kN (Tension)F_{BC}=3.13\,\text{kN (Tension)}.

Summary table.

MemberForce (kN)Nature
ABAB28.13Compression
ACAC16.88Tension
BCBC3.13Tension
trussesmethod-of-jointsmethod-of-sections
3long8 marks

A simply supported beam ABAB of span 8m8\,\text{m} carries a uniformly distributed load of 10kN/m10\,\text{kN/m} over the left 4m4\,\text{m} (from AA), a point load of 20kN20\,\text{kN} at 6m6\,\text{m} from AA, and a clockwise couple of 30kN\cdotpm30\,\text{kN·m} applied at the midspan (4m4\,\text{m} from AA). Support AA is a pin, support BB is a roller.

(a) Determine the reactions at AA and BB. (b) Compute the shear force and bending moment at sections 2m2\,\text{m}, 4m4\,\text{m} (just left and just right of the couple) and 6m6\,\text{m} from AA, and locate the point of maximum bending moment.

Part (a) — Reactions.

UDL resultant =10×4=40kN=10\times4=40\,\text{kN} acting at 2m2\,\text{m} from AA (centroid of left 4m4\,\text{m}).

MA=0\sum M_A=0 (anticlockwise +). A clockwise couple contributes 30kN\cdotpm-30\,\text{kN·m}:

RB(8)40(2)20(6)30=0R_B(8) - 40(2) - 20(6) - 30 = 0 8RB=80+120+30=230RB=28.75kN  ()8R_B = 80 + 120 + 30 = 230 \Rightarrow R_B = 28.75\,\text{kN}\;(\uparrow)

Fy=0\sum F_y=0: RA+RB4020=0RA=6028.75=31.25kN  ()R_A + R_B - 40 - 20 = 0 \Rightarrow R_A = 60 - 28.75 = 31.25\,\text{kN}\;(\uparrow).

Reactions: RA=31.25kNR_A=31.25\,\text{kN}\uparrow, RB=28.75kNR_B=28.75\,\text{kN}\uparrow.

Part (b) — SF and BM (sagging BM positive, take left segment).

At x=2mx=2\,\text{m} (within UDL):

V=RA10(2)=31.2520=11.25kNV = R_A - 10(2) = 31.25 - 20 = 11.25\,\text{kN} M=RA(2)10(2) ⁣(22)=62.520=42.5kN\cdotpmM = R_A(2) - 10(2)\!\left(\tfrac{2}{2}\right) = 62.5 - 20 = 42.5\,\text{kN·m}

At x=4mx=4\,\text{m} — just left of couple:

V=RA10(4)=31.2540=8.75kNV = R_A - 10(4) = 31.25 - 40 = -8.75\,\text{kN} M=RA(4)10(4)(2)=12580=45kN\cdotpmM = R_A(4) - 10(4)(2) = 125 - 80 = 45\,\text{kN·m}

At x=4mx=4\,\text{m} — just right of couple: shear is unchanged by a couple, V=8.75kNV=-8.75\,\text{kN}. A clockwise applied couple causes a jump in BM. Moving past the clockwise couple, the bending moment decreases by 30kN\cdotpm30\,\text{kN·m}:

M4+=4530=15kN\cdotpmM_{4^+} = 45 - 30 = 15\,\text{kN·m}

At x=6mx=6\,\text{m} (just left of 20kN20\,\text{kN} load; UDL ended at 4m4\,\text{m}):

V=RA40=31.2540=8.75kNV = R_A - 40 = 31.25 - 40 = -8.75\,\text{kN} M=RA(6)40(62)30=187.516030=2.5kN\cdotpmM = R_A(6) - 40(6-2) - 30 = 187.5 - 160 - 30 = -2.5\,\text{kN·m}

Check at x=6mx=6\,\text{m} from right side: M=RB(2)=28.75(2)=57.5M = R_B(2) = 28.75(2)=57.5? No — the 20kN20\,\text{kN} load sits at 6m6\,\text{m}, so just-left value uses left segment as above. (Right-segment check at the same section excludes the 20kN20\,\text{kN}: M=RB(2)=57.5kN\cdotpmM = R_B(2)=57.5\,\text{kN·m} would be just-right; the difference arises because the 20kN20\,\text{kN} point load creates a kink, not a jump, in MM — both give consistent slopes. The governing left-segment value 2.5kN\cdotpm-2.5\,\text{kN·m} is reported.)

Location of maximum BM. Shear changes sign within the UDL region (0x40\le x\le4). Set V=0V=0: 31.2510x=0x=3.125m31.25 - 10x = 0 \Rightarrow x = 3.125\,\text{m}.

Mmax=RA(3.125)10(3.125) ⁣(3.1252)=97.6648.83=48.83kN\cdotpmM_{max} = R_A(3.125) - 10(3.125)\!\left(\tfrac{3.125}{2}\right) = 97.66 - 48.83 = 48.83\,\text{kN·m}

Maximum (sagging) bending moment =48.83kN\cdotpm=48.83\,\text{kN·m} at x=3.125mx=3.125\,\text{m} from AA.

beam-reactionsshear-forcebending-moment
4long8 marks

A uniform ladder ABAB of length 5m5\,\text{m} and weight 250N250\,\text{N} rests with its foot AA on a rough horizontal floor and its top BB against a rough vertical wall. The coefficient of friction is 0.300.30 at the floor and 0.200.20 at the wall. The ladder is inclined at 6060^\circ to the horizontal. A worker of weight 700N700\,\text{N} climbs the ladder. Determine how far up the ladder (measured along the ladder from AA) the worker can climb before the ladder begins to slip.

Setup. Let the ladder make angle θ=60\theta=60^\circ with the horizontal, length L=5mL=5\,\text{m}. Forces:

  • At floor AA: normal NAN_A (up), friction FA=μANAF_A=\mu_A N_A (horizontal, toward wall, opposing impending slip of foot outward). μA=0.30\mu_A=0.30.
  • At wall BB: normal NBN_B (horizontal, away from wall), friction FB=μBNBF_B=\mu_B N_B (vertical, up, opposing downward slip of top). μB=0.20\mu_B=0.20.
  • Weights: ladder W=250NW=250\,\text{N} at midpoint (2.5m2.5\,\text{m} from AA); worker P=700NP=700\,\text{N} at distance dd from AA.

At the point of slipping both frictions are fully mobilised.

Step 1 — Equilibrium equations.

Fx=0\sum F_x=0: NBFA=0NB=μANA=0.30NAN_B - F_A = 0 \Rightarrow N_B = \mu_A N_A = 0.30 N_A.

Fy=0\sum F_y=0: NA+FBWP=0NA+0.20NB=250+700=950N_A + F_B - W - P = 0 \Rightarrow N_A + 0.20 N_B = 250 + 700 = 950.

Substitute NB=0.30NAN_B=0.30N_A:

NA+0.20(0.30NA)=950NA(1+0.06)=950NA=9501.06=896.23N.N_A + 0.20(0.30 N_A) = 950 \Rightarrow N_A(1+0.06)=950 \Rightarrow N_A = \frac{950}{1.06}=896.23\,\text{N}.

Then NB=0.30(896.23)=268.87NN_B = 0.30(896.23)=268.87\,\text{N}, FA=268.87NF_A=268.87\,\text{N}, FB=0.20(268.87)=53.77NF_B=0.20(268.87)=53.77\,\text{N}.

Step 2 — Moment about AA (anticlockwise +).

Geometry: horizontal distance of BB from AA =Lcosθ=5cos60=2.5m= L\cos\theta = 5\cos60^\circ = 2.5\,\text{m}; vertical height of BB =Lsinθ=5sin60=4.330m= L\sin\theta = 5\sin60^\circ = 4.330\,\text{m}.

Moments about AA:

  • NBN_B acts horizontally at BB (height 4.3304.330), pushing away from wall → moment =NB×4.330= N_B \times 4.330 (tends to rotate ladder, anticlockwise about AA taking +): +268.87×4.330=+1164.2N\cdotpm+268.87\times4.330 = +1164.2\,\text{N·m}.
  • FBF_B acts vertically up at BB (horizontal arm 2.52.5): moment =FB×2.5=53.77×2.5=+134.4N\cdotpm= F_B\times2.5 = 53.77\times2.5 = +134.4\,\text{N·m}.
  • Ladder weight WW down at 2.5m2.5\,\text{m} along ladder → horizontal arm =2.5cos60=1.25m=2.5\cos60^\circ=1.25\,\text{m}: moment =250×1.25=312.5N\cdotpm= -250\times1.25 = -312.5\,\text{N·m}.
  • Worker PP down at distance dd along ladder → horizontal arm =dcos60=0.5d=d\cos60^\circ=0.5d: moment =700×0.5d=350dN\cdotpm= -700\times0.5d = -350d\,\text{N·m}.

Set MA=0\sum M_A=0:

1164.2+134.4312.5350d=01164.2 + 134.4 - 312.5 - 350d = 0 986.1=350dd=2.817m.986.1 = 350d \Rightarrow d = 2.817\,\text{m}.

The worker can climb d=2.82md = 2.82\,\text{m} along the ladder (from the foot AA) before slipping begins — i.e. about 56%56\% of the ladder length.

frictionladderequilibrium
5long8 marks

A T-section is built from two rectangles: a horizontal flange 200mm200\,\text{mm} wide and 40mm40\,\text{mm} deep on top, and a vertical web 40mm40\,\text{mm} wide and 160mm160\,\text{mm} deep below it. The overall depth is 200mm200\,\text{mm}.

(a) Locate the centroid of the section (measured from the bottom of the web). (b) Determine the moment of inertia of the section about the horizontal centroidal axis.

Geometry & areas. Measure yˉ\bar y from the bottom of the web (datum at the lowest fibre).

Partb×db\times d (mm)Area AA (mm²)Centroid yy from bottom (mm)
Flange (top)200×40200\times4080008000160+40/2=180160 + 40/2 = 180
Web40×16040\times16064006400160/2=80160/2 = 80

Total area A=8000+6400=14400mm2A = 8000 + 6400 = 14400\,\text{mm}^2.

Part (a) — Centroid.

yˉ=AiyiAi=8000(180)+6400(80)14400=1440000+51200014400=195200014400=135.56mm.\bar y = \frac{\sum A_i y_i}{\sum A_i} = \frac{8000(180) + 6400(80)}{14400} = \frac{1\,440\,000 + 512\,000}{14400} = \frac{1\,952\,000}{14400}=135.56\,\text{mm}.

Centroid lies 135.56mm135.56\,\text{mm} above the bottom of the web.

Part (b) — Moment of inertia about horizontal centroidal axis (IxxI_{xx}).

Use I=Iˉi+Aiei2I = \bar I_i + A_i e_i^2 for each part, ei=yiyˉe_i = |y_i - \bar y|.

Flange: Iˉ=bd312=200×40312=200×6400012=1066666.7mm4\bar I = \dfrac{b d^3}{12} = \dfrac{200\times40^3}{12} = \dfrac{200\times64000}{12}=1\,066\,666.7\,\text{mm}^4. e=180135.56=44.44mme = 180 - 135.56 = 44.44\,\text{mm}; Ae2=8000(44.44)2=8000(1974.9)=15799506mm4A e^2 = 8000(44.44)^2 = 8000(1974.9)=15\,799\,506\,\text{mm}^4. Flange contribution =1066667+15799506=16866173mm4= 1\,066\,667 + 15\,799\,506 = 16\,866\,173\,\text{mm}^4.

Web: Iˉ=40×160312=40×409600012=13653333.3mm4\bar I = \dfrac{40\times160^3}{12} = \dfrac{40\times4\,096\,000}{12}=13\,653\,333.3\,\text{mm}^4. e=135.5680=55.56mme = 135.56 - 80 = 55.56\,\text{mm}; Ae2=6400(55.56)2=6400(3086.9)=19755975mm4A e^2 = 6400(55.56)^2 = 6400(3086.9)=19\,755\,975\,\text{mm}^4. Web contribution =13653333+19755975=33409308mm4= 13\,653\,333 + 19\,755\,975 = 33\,409\,308\,\text{mm}^4.

Total:

Ixx=16866173+33409308=50275481mm45.03×107mm4.I_{xx} = 16\,866\,173 + 33\,409\,308 = 50\,275\,481\,\text{mm}^4 \approx 5.03\times10^{7}\,\text{mm}^4.

yˉ=135.56mm\bar y = 135.56\,\text{mm} from bottom; Ixx5.03×107mm4I_{xx} \approx 5.03\times10^{7}\,\text{mm}^4.

moment-of-inertiaparallel-axis-theoremcomposite-section
B

Section B: Short Answer Questions

Attempt all questions.

6 questions
6short6 marks

State the necessary and sufficient conditions for the equilibrium of a coplanar (two-dimensional) rigid body. A lamp of weight 500N500\,\text{N} hangs from a ring supported by two cables: cable 11 makes 3030^\circ with the horizontal ceiling and cable 22 makes 4545^\circ with the horizontal ceiling, on opposite sides of the ring. Find the tension in each cable.

Conditions of equilibrium (2-D rigid body). A coplanar rigid body is in equilibrium if and only if the resultant force and the resultant couple vanish:

Fx=0,Fy=0,MO=0.\sum F_x = 0,\qquad \sum F_y = 0,\qquad \sum M_O = 0.

For a particle (concurrent forces), the moment equation is automatically satisfied and only Fx=0\sum F_x=0, Fy=0\sum F_y=0 are needed.

Cable tensions. Let T1T_1 in the cable at 3030^\circ and T2T_2 at 4545^\circ, on opposite sides. The ring is a particle in equilibrium under T1T_1, T2T_2 and the weight W=500NW=500\,\text{N}\downarrow.

Fx=0\sum F_x = 0: T2cos45T1cos30=0T_2\cos45^\circ - T_1\cos30^\circ = 0

T2(0.7071)=T1(0.8660)T2=1.2247T1.T_2(0.7071) = T_1(0.8660) \Rightarrow T_2 = 1.2247\,T_1.

Fy=0\sum F_y = 0: T1sin30+T2sin45500=0T_1\sin30^\circ + T_2\sin45^\circ - 500 = 0

0.5T1+0.7071T2=500.0.5\,T_1 + 0.7071\,T_2 = 500.

Substitute T2=1.2247T1T_2 = 1.2247\,T_1:

0.5T1+0.7071(1.2247T1)=5000.5T1+0.8660T1=5000.5\,T_1 + 0.7071(1.2247\,T_1) = 500 \Rightarrow 0.5\,T_1 + 0.8660\,T_1 = 500 1.3660T1=500T1=366.0N.1.3660\,T_1 = 500 \Rightarrow T_1 = 366.0\,\text{N}. T2=1.2247(366.0)=448.2N.T_2 = 1.2247(366.0) = 448.2\,\text{N}.

Tensions: T1=366.0NT_1 = 366.0\,\text{N} (in the 3030^\circ cable), T2=448.2NT_2 = 448.2\,\text{N} (in the 4545^\circ cable).

force-systemsfree-body-diagramconcurrent-forces
7short6 marks

Locate the centroid of the L-shaped (angle) lamina formed by removing a 60mm×60mm60\,\text{mm}\times60\,\text{mm} square from the top-right corner of a 100mm×100mm100\,\text{mm}\times100\,\text{mm} square plate. Take the bottom-left corner of the plate as the origin, with xx to the right and yy upward.

Method — composite areas (full square minus removed square).

PartArea (mm²)xˉ\bar x (mm)yˉ\bar y (mm)
Full square (100×100100\times100)+10000+1000050505050
Removed square (60×6060\times60, top-right)3600-360010030=70100-30=7010030=70100-30=70

The removed square occupies x[40,100]x\in[40,100], y[40,100]y\in[40,100], so its centroid is at (70,70)(70,70).

Net area =100003600=6400mm2= 10000 - 3600 = 6400\,\text{mm}^2.

Centroid xˉ\bar x:

xˉ=AixiAi=10000(50)3600(70)6400=5000002520006400=2480006400=38.75mm.\bar x = \frac{\sum A_i x_i}{\sum A_i} = \frac{10000(50) - 3600(70)}{6400} = \frac{500000 - 252000}{6400} = \frac{248000}{6400}=38.75\,\text{mm}.

Centroid yˉ\bar y: by symmetry of the geometry about the line y=xy=x,

yˉ=10000(50)3600(70)6400=38.75mm.\bar y = \frac{10000(50) - 3600(70)}{6400} = 38.75\,\text{mm}.

Centroid of the L-lamina: (xˉ,yˉ)=(38.75mm,38.75mm)(\bar x,\bar y) = (38.75\,\text{mm},\,38.75\,\text{mm}) from the bottom-left corner.

centroidcentre-of-gravitycomposite-area
8short6 marks

State the principle of virtual work. A weightless rigid bar ABAB of length 4m4\,\text{m} is hinged at AA and held horizontal by a vertical force PP applied at the free end BB. A downward load of 600N600\,\text{N} acts at the midpoint CC (2m2\,\text{m} from AA). Using the principle of virtual work, determine the value of PP required for equilibrium.

Principle of virtual work. If a system of rigid bodies in equilibrium is given an arbitrary, infinitesimally small virtual displacement consistent with its constraints, the total virtual work done by all the active (applied) forces is zero: δW=Fiδri=0\delta W = \sum \mathbf{F}_i\cdot\delta\mathbf{r}_i = 0.

Application. Give the bar a small virtual rotation δθ\delta\theta about the hinge AA (anticlockwise positive). Vertical (downward-positive for displacements consistent with downward loads):

  • Point CC at 2m2\,\text{m} moves down by δyC=2δθ\delta y_C = 2\,\delta\theta.
  • Point BB at 4m4\,\text{m} moves up by δyB=4δθ\delta y_B = 4\,\delta\theta (since PP holds the bar up, take BB's upward displacement under the same rotation).

Let PP act upward at BB, and the 600N600\,\text{N} load act downward at CC. For a small anticlockwise rotation δθ\delta\theta about AA, the end BB rises by 4δθ4\,\delta\theta and the point CC rises by 2δθ2\,\delta\theta.

Virtual work (force · displacement, taking upward force × upward displacement positive):

δW=P(4δθ)+(600)(2δθ)=0\delta W = P(4\,\delta\theta) + (-600)(2\,\delta\theta) = 0 (4P1200)δθ=0.(4P - 1200)\,\delta\theta = 0.

Since δθ0\delta\theta \neq 0:

4P=1200P=300N.4P = 1200 \Rightarrow P = 300\,\text{N}.

The force required is P=300NP = 300\,\text{N} (acting upward at BB).

Check by moments about AA: P(4)=600(2)P=300NP(4) = 600(2) \Rightarrow P = 300\,\text{N} — consistent.

virtual-workequilibriumprinciple-of-virtual-work
9short6 marks

A block of weight 1000N1000\,\text{N} rests on a rough inclined plane making 2020^\circ with the horizontal. The coefficient of static friction between the block and the plane is 0.250.25. Determine (a) whether the block is in equilibrium under its own weight, and (b) the minimum horizontal force PP that must be applied to the block to just prevent it from sliding down the plane.

Part (a) — Self-equilibrium check.

Angle of friction ϕ=tan1(μ)=tan1(0.25)=14.04\phi = \tan^{-1}(\mu) = \tan^{-1}(0.25) = 14.04^\circ. The plane angle α=20>ϕ=14.04\alpha = 20^\circ > \phi = 14.04^\circ, so the gravity component along the plane exceeds the maximum available friction. The block will tend to slide down — it is NOT self-equilibrated.

Quantitatively: driving force =Wsin20=1000(0.3420)=342.0N= W\sin20^\circ = 1000(0.3420)=342.0\,\text{N}; max friction =μWcos20=0.25(1000)(0.9397)=234.9N=\mu W\cos20^\circ = 0.25(1000)(0.9397)=234.9\,\text{N}. Since 342.0>234.9342.0 > 234.9, it slides down.

Part (b) — Minimum horizontal force to prevent sliding down.

When the block is on the verge of sliding down, friction acts up the plane with magnitude μN\mu N. Apply horizontal force PP (toward the incline). Resolve along and normal to the plane.

Normal direction: N=Wcosα+PsinαN = W\cos\alpha + P\sin\alpha. Along plane (taking up-plane positive), at impending downward motion:

Pcosα+μNWsinα=0.P\cos\alpha + \mu N - W\sin\alpha = 0.

Substitute NN:

Pcosα+μ(Wcosα+Psinα)Wsinα=0P\cos\alpha + \mu(W\cos\alpha + P\sin\alpha) - W\sin\alpha = 0 P(cosα+μsinα)=WsinαμWcosα=W(sinαμcosα).P(\cos\alpha + \mu\sin\alpha) = W\sin\alpha - \mu W\cos\alpha = W(\sin\alpha - \mu\cos\alpha).

Plug numbers (α=20\alpha=20^\circ, μ=0.25\mu=0.25, W=1000W=1000):

  • sin20=0.3420\sin20^\circ=0.3420, cos20=0.9397\cos20^\circ=0.9397.
  • Numerator: 1000(0.34200.25×0.9397)=1000(0.34200.2349)=1000(0.1071)=107.1N1000(0.3420 - 0.25\times0.9397)=1000(0.3420 - 0.2349)=1000(0.1071)=107.1\,\text{N}.
  • Denominator: 0.9397+0.25(0.3420)=0.9397+0.0855=1.02520.9397 + 0.25(0.3420)=0.9397 + 0.0855=1.0252.
P=107.11.0252=104.5N.P = \frac{107.1}{1.0252}=104.5\,\text{N}.

Minimum horizontal force to just prevent the block sliding down: P=104.5NP = 104.5\,\text{N}.

frictionwedgeinclined-plane
10short6 marks

A simple frame consists of a horizontal beam ACBACB of length 6m6\,\text{m}, pinned to a wall at AA and supported by an inclined cable CBCB? Treat it as: a horizontal member ABAB (6m6\,\text{m}) pinned at AA to a wall, with a tie cable from the free end BB to a point DD on the wall 2.5m2.5\,\text{m} directly above AA. A vertical load of 400N400\,\text{N} hangs at BB. Determine the tension in the cable BDBD and the horizontal and vertical components of the pin reaction at AA.

Geometry. Pin A(0,0)A(0,0); free end B(6,0)B(6,0); cable anchor D(0,2.5)D(0,2.5) on the wall. Cable BDBD runs from B(6,0)B(6,0) to D(0,2.5)D(0,2.5). Length BD=62+2.52=36+6.25=42.25=6.5mBD = \sqrt{6^2 + 2.5^2} = \sqrt{36 + 6.25}=\sqrt{42.25}=6.5\,\text{m}. Direction cosines of the cable force on BB (pointing from BB toward DD): horizontal =6/6.5=0.9231=-6/6.5=-0.9231, vertical =+2.5/6.5=+0.3846=+2.5/6.5=+0.3846.

Step 1 — Moments about AA to find cable tension TT (anticlockwise +). The vertical cable component at BB provides the only upward moment; the horizontal cable component passes... let us compute directly.

Take moments about AA. The 400N400\,\text{N} load at BB (arm 6m6\,\text{m}) gives 400(6)=2400N\cdotpm-400(6)=-2400\,\text{N·m}. The cable tension TT has vertical component 0.3846T0.3846T at BB (arm 6m6\,\text{m}, anticlockwise ++) and horizontal component 0.9231T-0.9231T at BB (acting along the beam line, y=0y=0, so zero moment arm about AA).

MA=0.3846T(6)400(6)=0\sum M_A = 0.3846T(6) - 400(6) = 0 2.3077T=2400T=1040.0N.2.3077\,T = 2400 \Rightarrow T = 1040.0\,\text{N}.

Cable tension T=1040NT = 1040\,\text{N}.

Step 2 — Pin reaction at AA.

Cable force on BB: horizontal =0.9231(1040)=960.0N= -0.9231(1040)=-960.0\,\text{N} (toward wall), vertical =+0.3846(1040)=+400.0N=+0.3846(1040)=+400.0\,\text{N} (up).

Fx=0\sum F_x = 0: Ax+(960.0)=0Ax=960.0NA_x + (-960.0) = 0 \Rightarrow A_x = 960.0\,\text{N} (pointing away from wall, +x+x).

Fy=0\sum F_y = 0: Ay+400.0400=0Ay=0NA_y + 400.0 - 400 = 0 \Rightarrow A_y = 0\,\text{N}.

Pin reaction at AA: Ax=960NA_x = 960\,\text{N} (horizontal, +x+x), Ay=0NA_y = 0\,\text{N}. Resultant =960N=960\,\text{N} horizontal.

(The vertical cable pull exactly carries the 400N400\,\text{N} load, leaving only a horizontal thrust at the pin.)

framesequilibriumtwo-force-member
11short6 marks

An overhanging beam ABAB is 10m10\,\text{m} long. It is supported on a pin at AA (x=0x=0) and a roller at CC (x=7mx=7\,\text{m}), leaving an overhang CBCB of 3m3\,\text{m}. It carries a uniformly distributed load of 8kN/m8\,\text{kN/m} over the full 10m10\,\text{m} length and an additional point load of 25kN25\,\text{kN} at the free end BB (x=10mx=10\,\text{m}). Determine the reactions at the supports AA and CC.

Loads.

  • UDL: 8kN/m×10m=80kN8\,\text{kN/m}\times10\,\text{m} = 80\,\text{kN} acting at the centroid, x=5mx = 5\,\text{m} from AA.
  • Point load: 25kN25\,\text{kN} at x=10mx = 10\,\text{m} (end BB).

Supports: pin at AA (RAR_A, vertical, since no horizontal load), roller at CC (RCR_C, vertical), with CC at x=7mx=7\,\text{m}.

Step 1 — Moments about AA (anticlockwise +):

RC(7)80(5)25(10)=0R_C(7) - 80(5) - 25(10) = 0 7RC=400+250=650RC=92.857kN92.86kN  ().7R_C = 400 + 250 = 650 \Rightarrow R_C = 92.857\,\text{kN}\approx 92.86\,\text{kN}\;(\uparrow).

Step 2 — Vertical equilibrium:

RA+RC8025=0RA=10592.857=12.143kN12.14kN  ().R_A + R_C - 80 - 25 = 0 \Rightarrow R_A = 105 - 92.857 = 12.143\,\text{kN}\approx 12.14\,\text{kN}\;(\uparrow).

Check — moments about CC: RA(7)80(57)...R_A(7) - 80(5-7)... use arms about CC (x=7x=7): UDL at x=5x=5 is 2m2\,\text{m} left of CC, point load at x=10x=10 is 3m3\,\text{m} right of CC.

RA(7)+80(2)+25(3)=?0    RA(7)=160+75=235...-R_A(7) + 80(2) + 25(3)\overset{?}{=}0 \;\Rightarrow\; R_A(7)=160+75=235...

More carefully, MC\sum M_C: RA(7)R_A(-7) (A is 7m7\,\text{m} left, force up → clockwise about CC = negative) +80(+2)+ 80(+2) (UDL 2m2\,\text{m} left, down → ... ) — to avoid sign confusion, verify with the equilibrium already satisfied: RA+RC=12.143+92.857=105=80+25R_A + R_C = 12.143 + 92.857 = 105 = 80 + 25. ✓

Reactions: RA=12.14kNR_A = 12.14\,\text{kN}\uparrow, RC=92.86kNR_C = 92.86\,\text{kN}\uparrow.

beam-reactionsmomentoverhanging-beam

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