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A

Section A: Long Answer Questions

Attempt all questions.

5 questions
1long10 marks

Four coplanar concurrent forces act at point OO as shown. Their magnitudes and directions (measured anticlockwise from the positive xx-axis) are:

ForceMagnitude (N)Angle
F1F_12003030^\circ
F2F_2150110110^\circ
F3F_3120200200^\circ
F4F_4180300300^\circ

Determine the magnitude and direction of the resultant of this force system, and state the single force needed to keep the point in equilibrium (the equilibrant).

Method: Resolve every force into rectangular components, sum them, then recombine.

Fx=Fcosθ,Fy=FsinθF_x = F\cos\theta,\qquad F_y = F\sin\theta

Component table

ForceFcosθF\cos\theta (N)FsinθF\sin\theta (N)
F1=200F_1=200 at 3030^\circ200cos30=+173.21200\cos30^\circ = +173.21200sin30=+100.00200\sin30^\circ = +100.00
F2=150F_2=150 at 110110^\circ150cos110=51.30150\cos110^\circ = -51.30150sin110=+140.95150\sin110^\circ = +140.95
F3=120F_3=120 at 200200^\circ120cos200=112.76120\cos200^\circ = -112.76120sin200=41.04120\sin200^\circ = -41.04
F4=180F_4=180 at 300300^\circ180cos300=+90.00180\cos300^\circ = +90.00180sin300=155.88180\sin300^\circ = -155.88

Sum of components

Fx=173.2151.30112.76+90.00=+99.15 N\sum F_x = 173.21 - 51.30 - 112.76 + 90.00 = +99.15\ \text{N} Fy=100.00+140.9541.04155.88=+44.03 N\sum F_y = 100.00 + 140.95 - 41.04 - 155.88 = +44.03\ \text{N}

Magnitude of resultant

R=(Fx)2+(Fy)2=99.152+44.032=9830.7+1938.6=11769.3=108.49 NR = \sqrt{(\sum F_x)^2 + (\sum F_y)^2} = \sqrt{99.15^2 + 44.03^2} = \sqrt{9830.7 + 1938.6} = \sqrt{11769.3} = 108.49\ \text{N}

Direction (measured anticlockwise from +x+x, both components positive so resultant lies in the first quadrant):

θ=tan1 ⁣(FyFx)=tan1 ⁣(44.0399.15)=tan1(0.4441)=23.95\theta = \tan^{-1}\!\left(\frac{\sum F_y}{\sum F_x}\right) = \tan^{-1}\!\left(\frac{44.03}{99.15}\right) = \tan^{-1}(0.4441) = 23.95^\circ

Resultant: R=108.49 N at 23.95 from +x-axis\boxed{R = 108.49\ \text{N at } 23.95^\circ \text{ from } +x\text{-axis}}

Equilibrant: equal in magnitude but opposite in sense, i.e. 108.49 N at 203.95\boxed{108.49\ \text{N at } 203.95^\circ} (i.e. 23.9523.95^\circ below the negative xx-axis). It exactly cancels the resultant, leaving the point in equilibrium.

force-systemsresultantconcurrent-forces
2long10 marks

A simply supported plane truss spans 6m6\,\text{m} between supports AA (pin) and BB (roller). It consists of two equilateral triangles. Joints along the bottom chord are AA, CC, BB with AC=CB=3mAC = CB = 3\,\text{m}; the apex joint DD is at the top. Members are ACAC, CBCB (bottom), ADAD, DBDB (top inclined) and CDCD (vertical). Each inclined member makes 6060^\circ with the horizontal. A downward vertical load of 40kN40\,\text{kN} is applied at apex DD.

Determine the support reactions and the force in every member, stating whether each is in tension or compression.

Geometry: AC=CB=3mAC=CB=3\,\text{m}, apex DD above CC. Inclined members ADAD and DBDB at 6060^\circ to the horizontal. Height of DD: h=3tan60h = 3\tan60^\circ... actually with equilateral triangles of side 3m3\,\text{m} the apex is above CC at height h=3sin60×h = 3\sin60^\circ \times — let us use the member geometry directly: ADAD runs from A(0,0)A(0,0) to D(3,h)D(3, h). For an equilateral triangle on base AC=3AC=3, D=(1.5,1.5tan60)=(1.5,2.598)D=(1.5, 1.5\tan60^\circ)=(1.5,2.598). Re-reading: the two equilateral triangles share apex region; standard king-post form gives DD above midspan C(3,0)C(3,0) with ADAD, DBDB at 6060^\circ. Take D=(3,3tan60)=(3,5.196)D=(3, 3\tan60^\circ)=(3,5.196) so that ADAD makes 6060^\circ with horizontal. We adopt this consistent geometry: A(0,0)A(0,0), C(3,0)C(3,0), B(6,0)B(6,0), D(3,5.196)D(3,5.196).

Support reactions (symmetry, load 40 kN at DD over midspan):

MA=0: RB(6)40(3)=0RB=20 kN (up)\sum M_A = 0:\ R_B(6) - 40(3) = 0 \Rightarrow R_B = 20\ \text{kN (up)} Fy=0: RAy=4020=20 kN (up)\sum F_y = 0:\ R_{Ay} = 40 - 20 = 20\ \text{kN (up)} Fx=0: RAx=0\sum F_x = 0:\ R_{Ax}=0

Joint A (members ACAC horizontal, ADAD at 6060^\circ above horizontal). Let tension positive.

Fy=0: RAy+FADsin60=0FAD=20sin60=200.8660=23.09 kN\sum F_y=0:\ R_{Ay} + F_{AD}\sin60^\circ = 0 \Rightarrow F_{AD} = -\frac{20}{\sin60^\circ} = -\frac{20}{0.8660} = -23.09\ \text{kN}

Negative \Rightarrow compression. FAD=23.09 kN (C)F_{AD}=23.09\ \text{kN (C)}.

Fx=0: FAC+FADcos60=0FAC=(23.09)(0.5)=+11.55 kN\sum F_x=0:\ F_{AC} + F_{AD}\cos60^\circ = 0 \Rightarrow F_{AC} = -(-23.09)(0.5) = +11.55\ \text{kN}

Positive \Rightarrow tension. FAC=11.55 kN (T)F_{AC}=11.55\ \text{kN (T)}.

Joint B (by symmetry): FDB=23.09 kN (C)F_{DB}=23.09\ \text{kN (C)}, FCB=11.55 kN (T)F_{CB}=11.55\ \text{kN (T)}.

Joint C (members ACAC, CBCB horizontal; CDCD vertical). No external load at CC.

Fy=0: FCD+0=0FCD=0 (zero-force member)\sum F_y=0:\ F_{CD} + 0 = 0 \Rightarrow F_{CD}=0\ \text{(zero-force member)}

(Check Fx\sum F_x at C: FCBFAC=11.5511.55=0F_{CB}-F_{AC}=11.55-11.55=0. OK.)

Verification at apex D (members ADAD, DBDB, CDCD, load 40 kN down):

Fy=40+FADsin60(toward A, compression pushes up)+FDBsin60=40+23.09(0.866)+23.09(0.866)=40+40.0=0 \sum F_y = -40 + F_{AD}\sin60^\circ\,(\text{toward }A,\ \text{compression pushes up}) + F_{DB}\sin60^\circ = -40 + 23.09(0.866) + 23.09(0.866) = -40 + 40.0 = 0\ \checkmark

Summary of member forces

MemberForce (kN)Nature
ACAC11.55Tension
CBCB11.55Tension
ADAD23.09Compression
DBDB23.09Compression
CDCD0Zero-force

Reactions: RA=20 kNR_A = 20\ \text{kN}\uparrow, RB=20 kNR_B = 20\ \text{kN}\uparrow.

trussesmethod-of-jointsequilibrium
3long10 marks

A simply supported beam ABAB of span 8m8\,\text{m} carries:

  • A point load of 30kN30\,\text{kN} at 2m2\,\text{m} from AA.
  • A uniformly distributed load (UDL) of 10kN/m10\,\text{kN/m} over the 4m4\,\text{m} length from 4m4\,\text{m} to 8m8\,\text{m} (i.e. up to support BB).

Support AA is a pin and BB is a roller. (a) Find the reactions at AA and BB. (b) Draw the shear force diagram (SFD) and bending moment diagram (BMD), giving salient values. (c) Locate the point of maximum bending moment and compute its value.

Total loads: point load P=30kNP=30\,\text{kN} at x=2mx=2\,\text{m}; UDL =10×4=40kN=10\times4 = 40\,\text{kN} acting at its centroid, x=4+4/2=6mx = 4 + 4/2 = 6\,\text{m}.

(a) Reactions

MA=0: RB(8)30(2)40(6)=0RB=60+2408=3008=37.5 kN\sum M_A = 0:\ R_B(8) - 30(2) - 40(6) = 0 \Rightarrow R_B = \frac{60 + 240}{8} = \frac{300}{8} = 37.5\ \text{kN} Fy=0: RA=(30+40)37.5=7037.5=32.5 kN\sum F_y = 0:\ R_A = (30+40) - 37.5 = 70 - 37.5 = 32.5\ \text{kN} RA=32.5 kN,RB=37.5 kN\boxed{R_A = 32.5\ \text{kN},\quad R_B = 37.5\ \text{kN}}

(b) Shear force (from left, downward loads negative):

  • Just right of AA: V=+32.5 kNV = +32.5\ \text{kN}
  • Just left of point load (x=2x=2^-): V=+32.5 kNV = +32.5\ \text{kN}
  • Just right of point load (x=2+x=2^+): V=32.530=+2.5 kNV = 32.5 - 30 = +2.5\ \text{kN}
  • From x=2x=2 to x=4x=4 no load: stays +2.5 kN+2.5\ \text{kN}
  • Over UDL (4x84\le x\le8): V(x)=2.510(x4)V(x) = 2.5 - 10(x-4).
    • At x=4x=4: V=+2.5 kNV=+2.5\ \text{kN}
    • At x=8x=8^-: V=2.510(4)=37.5 kNV = 2.5 - 10(4) = -37.5\ \text{kN} (jumps to 0 at RBR_B).

Shear crosses zero within the UDL: 2.510(x4)=0x4=0.25x=4.25 m2.5 - 10(x-4)=0 \Rightarrow x-4 = 0.25 \Rightarrow x = 4.25\ \text{m}.

Bending moments (sagging positive):

  • At AA: M=0M=0
  • At x=2x=2 (under point load): M=32.5(2)=65.0 kN\cdotpmM = 32.5(2) = 65.0\ \text{kN·m}
  • At x=4x=4 (start of UDL): M=32.5(4)30(42)=13060=70.0 kN\cdotpmM = 32.5(4) - 30(4-2) = 130 - 60 = 70.0\ \text{kN·m}
  • At x=4.25x=4.25 (zero shear, maximum):
M=32.5(4.25)30(4.252)10(4.254)22M = 32.5(4.25) - 30(4.25-2) - 10\frac{(4.25-4)^2}{2} =138.12530(2.25)10(0.25)22=138.12567.50.3125=70.31 kN\cdotpm= 138.125 - 30(2.25) - 10\frac{(0.25)^2}{2} = 138.125 - 67.5 - 0.3125 = 70.31\ \text{kN·m}
  • At BB: M=0M=0 (check).

(c) Maximum bending moment

Mmax=70.31 kN\cdotpm at x=4.25 m from A\boxed{M_{max} = 70.31\ \text{kN·m at } x = 4.25\ \text{m from }A}

SFD (ASCII sketch):

+32.5 ┐
      │   +2.5 ┐
  ────┘────────┼──────  (zero at x=4.25)
               └──────► -37.5 at B

BMD: rises linearly from 0 at A to 65 at x=2, to 70 at x=4, peaks 70.31 at x=4.25, then parabolic back to 0 at B. The diagram is entirely sagging (positive).

beam-reactionsshear-forcebending-moment
4long8 marks

A T-section is built from two rectangles: a horizontal flange 120mm120\,\text{mm} wide ×20mm\times\,20\,\text{mm} deep sitting on top of a vertical web 20mm20\,\text{mm} wide ×100mm\times\,100\,\text{mm} deep. The overall depth is 120mm120\,\text{mm}.

Determine: (a) the location of the centroid measured from the bottom of the web, and (b) the moment of inertia of the whole section about the horizontal centroidal axis (IxxI_{xx}).

Subdivide into flange (1) and web (2). Reference: bottom of web (y=0y=0).

PartArea AA (mm²)yˉ\bar y from bottom (mm)AyˉA\bar y (mm³)
Flange 120×20120\times2024002400100+20/2=110100 + 20/2 = 110264000264000
Web 20×10020\times10020002000100/2=50100/2 = 50100000100000
Total44004400364000364000

(a) Centroid

Yˉ=AyˉA=3640004400=82.73 mm from bottom of web\bar Y = \frac{\sum A\bar y}{\sum A} = \frac{364000}{4400} = 82.73\ \text{mm from bottom of web} Yˉ=82.73 mm\boxed{\bar Y = 82.73\ \text{mm}}

(b) Moment of inertia about centroidal x-axis using I=Ig+Ad2I = I_g + A d^2 for each part, with d=yˉYˉd = |\bar y - \bar Y|.

Flange:

Ig1=bh312=120(20)312=120×800012=80000 mm4I_{g1} = \frac{b h^3}{12} = \frac{120(20)^3}{12} = \frac{120 \times 8000}{12} = 80000\ \text{mm}^4 d1=11082.73=27.27 mm,A1d12=2400(27.27)2=2400(743.65)=1784766 mm4d_1 = 110 - 82.73 = 27.27\ \text{mm},\quad A_1 d_1^2 = 2400(27.27)^2 = 2400(743.65) = 1\,784\,766\ \text{mm}^4 I1=80000+1784766=1864766 mm4I_1 = 80000 + 1\,784\,766 = 1\,864\,766\ \text{mm}^4

Web:

Ig2=20(100)312=20×10612=1666667 mm4I_{g2} = \frac{20(100)^3}{12} = \frac{20 \times 10^6}{12} = 1\,666\,667\ \text{mm}^4 d2=82.7350=32.73 mm,A2d22=2000(32.73)2=2000(1071.25)=2142500 mm4d_2 = 82.73 - 50 = 32.73\ \text{mm},\quad A_2 d_2^2 = 2000(32.73)^2 = 2000(1071.25) = 2\,142\,500\ \text{mm}^4 I2=1666667+2142500=3809167 mm4I_2 = 1\,666\,667 + 2\,142\,500 = 3\,809\,167\ \text{mm}^4

Total:

Ixx=I1+I2=1864766+3809167=5673933 mm4I_{xx} = I_1 + I_2 = 1\,864\,766 + 3\,809\,167 = 5\,673\,933\ \text{mm}^4 Ixx5.67×106 mm4\boxed{I_{xx} \approx 5.67 \times 10^{6}\ \text{mm}^4}
moment-of-inertiacomposite-sectionparallel-axis
5long8 marks

A uniform ladder 6m6\,\text{m} long weighs 250N250\,\text{N} and rests against a smooth vertical wall, with its foot on a rough horizontal floor. The ladder is inclined at 6060^\circ to the horizontal. The coefficient of friction between the ladder and the floor is μ=0.30\mu = 0.30. (a) Check whether the ladder is in equilibrium under its own weight. (b) Find the maximum distance (measured along the ladder from the foot) up which a person weighing 700N700\,\text{N} can climb before the ladder is about to slip.

Setup. Wall smooth \Rightarrow only a horizontal normal reaction NWN_W at the top. Floor rough \Rightarrow vertical normal NFN_F and friction F=μNFF = \mu N_F at the foot. Ladder length L=6mL=6\,\text{m}, angle θ=60\theta=60^\circ, weight W=250NW=250\,\text{N} at midpoint (3m3\,\text{m} along).

Let foot be the origin. Top is at horizontal distance Lcosθ=6cos60=3.0mL\cos\theta = 6\cos60^\circ = 3.0\,\text{m} and height Lsinθ=6sin60=5.196mL\sin\theta = 6\sin60^\circ = 5.196\,\text{m}.

(a) Ladder alone.

Fy=0: NF=W=250 N\sum F_y = 0:\ N_F = W = 250\ \text{N}

Taking moments about the foot (eliminates NFN_F and floor friction):

Mfoot=0: NW(Lsinθ)W(L2cosθ)=0\sum M_{foot}=0:\ N_W(L\sin\theta) - W\left(\tfrac{L}{2}\cos\theta\right) = 0 NW=W(L2cosθ)Lsinθ=W2cotθ=2502cot60=125×0.5774=72.17 NN_W = \frac{W(\tfrac{L}{2}\cos\theta)}{L\sin\theta} = \frac{W}{2}\cot\theta = \frac{250}{2}\cot60^\circ = 125 \times 0.5774 = 72.17\ \text{N}

Required friction at foot =NW=72.17 N= N_W = 72.17\ \text{N} (horizontal equilibrium). Maximum available friction =μNF=0.30×250=75.0 N= \mu N_F = 0.30 \times 250 = 75.0\ \text{N}.

Since required 72.17 N<75.0 N72.17\ \text{N} < 75.0\ \text{N} available, the ladder is in equilibrium (it does not slip) under its own weight. \checkmark

(b) Person of weight Wp=700NW_p = 700\,\text{N} at distance dd along the ladder.

Vertical equilibrium: NF=W+Wp=250+700=950 NN_F = W + W_p = 250 + 700 = 950\ \text{N}. At impending slip, friction is fully mobilised: F=μNF=0.30×950=285 NF = \mu N_F = 0.30 \times 950 = 285\ \text{N}. Horizontal equilibrium: NW=F=285 NN_W = F = 285\ \text{N}.

Moments about the foot (the person's weight acts at horizontal distance dcosθd\cos\theta):

NW(Lsinθ)=W(L2cosθ)+Wp(dcosθ)N_W(L\sin\theta) = W\left(\tfrac{L}{2}\cos\theta\right) + W_p(d\cos\theta) 285(5.196)=250(3.0cos60)+700dcos60285(5.196) = 250(3.0\cos60^\circ) + 700\,d\cos60^\circ

Compute: 285×5.196=1480.86285 \times 5.196 = 1480.86;  3.0cos60=1.5\ 3.0\cos60^\circ = 1.5, so 250×1.5=375250 \times 1.5 = 375;  cos60=0.5\ \cos60^\circ = 0.5.

1480.86=375+700(0.5)d=375+350d1480.86 = 375 + 700(0.5)d = 375 + 350\,d 350d=1480.86375=1105.86d=1105.86350=3.16 m350\,d = 1480.86 - 375 = 1105.86 \Rightarrow d = \frac{1105.86}{350} = 3.16\ \text{m} dmax=3.16 m along the ladder from the foot\boxed{d_{max} = 3.16\ \text{m along the ladder from the foot}}

This is just past the midpoint (3.0 m), so the person can climb a little above the centre before slipping is imminent.

frictionladder-frictionequilibrium
B

Section B: Short Answer Questions

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6 questions
6short6 marks

A plane lamina consists of a rectangle 80mm80\,\text{mm} wide ×60mm\times\,60\,\text{mm} tall, from which a circular hole of diameter 30mm30\,\text{mm} is removed. The centre of the hole is at (50,30)mm(50, 30)\,\text{mm} measured from the bottom-left corner of the rectangle. Locate the centroid of the remaining area.

Treat the hole as negative area. Reference: bottom-left corner (0,0)(0,0).

Rectangle: A1=80×60=4800 mm2A_1 = 80 \times 60 = 4800\ \text{mm}^2, centroid at (xˉ1,yˉ1)=(40,30) mm(\bar x_1,\bar y_1) = (40, 30)\ \text{mm}.

Hole (negative): A2=π4(30)2=π4(900)=706.86 mm2A_2 = -\dfrac{\pi}{4}(30)^2 = -\dfrac{\pi}{4}(900) = -706.86\ \text{mm}^2, centroid at (50,30) mm(50, 30)\ \text{mm}.

Net area: A=4800706.86=4093.14 mm2A = 4800 - 706.86 = 4093.14\ \text{mm}^2.

Xˉ=A1xˉ1+A2xˉ2A=4800(40)+(706.86)(50)4093.14=192000353434093.14=1566574093.14=38.27 mm\bar X = \frac{A_1\bar x_1 + A_2\bar x_2}{A} = \frac{4800(40) + (-706.86)(50)}{4093.14} = \frac{192000 - 35343}{4093.14} = \frac{156657}{4093.14} = 38.27\ \text{mm} Yˉ=4800(30)+(706.86)(30)4093.14=(4800706.86)(30)4093.14=4093.14×304093.14=30.0 mm\bar Y = \frac{4800(30) + (-706.86)(30)}{4093.14} = \frac{(4800 - 706.86)(30)}{4093.14} = \frac{4093.14 \times 30}{4093.14} = 30.0\ \text{mm}

(Yˉ=30\bar Y = 30 mm exactly, since both shapes are centred at y=30y=30.)

(Xˉ,Yˉ)=(38.27, 30.0) mm from the bottom-left corner\boxed{(\bar X,\bar Y) = (38.27,\ 30.0)\ \text{mm from the bottom-left corner}}
centroidcomposite-area
7short6 marks

Using the principle of virtual work, determine the reaction at the roller support BB of a simply supported beam ABAB of span 5m5\,\text{m} (AA is a pin, BB is a roller) carrying a single point load of 60kN60\,\text{kN} at 2m2\,\text{m} from AA.

Principle of virtual work: for a system in equilibrium, the total virtual work done by all active forces during any kinematically admissible virtual displacement is zero: δU=0\delta U = 0.

Remove the roller at BB and replace it by the unknown reaction RBR_B, treating it as an active force. Give the beam a small virtual rotation δθ\delta\theta about the pin AA (a rigid-body virtual displacement consistent with the pin constraint).

Virtual vertical displacements (upward positive):

  • At BB (x=5mx=5\,\text{m}): δB=5δθ\delta_B = 5\,\delta\theta (upward, in direction of RBR_B).
  • At the load point (x=2mx=2\,\text{m}): δL=2δθ\delta_L = 2\,\delta\theta (upward); the 60 kN load acts downward, so its virtual work is negative.

Virtual work equation:

δU=RB(5δθ)60(2δθ)=0\delta U = R_B(5\,\delta\theta) - 60(2\,\delta\theta) = 0

Divide by δθ (0)\delta\theta\ (\neq 0):

5RB120=0RB=1205=24 kN5R_B - 120 = 0 \Rightarrow R_B = \frac{120}{5} = 24\ \text{kN} RB=24 kN (upward)\boxed{R_B = 24\ \text{kN (upward)}}

Check (statics): MA=0: RB(5)=60(2)RB=24 kN.\sum M_A = 0:\ R_B(5) = 60(2) \Rightarrow R_B = 24\ \text{kN}. \checkmark

virtual-workequilibriumbeam-reactions
8short5 marks

A force of 100N100\,\text{N} acts at point P(4,3)mP(4, 3)\,\text{m} directed along the vector (3,4)(3, 4) (i.e. at angle tan1(4/3)\tan^{-1}(4/3) above the xx-axis). (a) Compute the moment of this force about the origin OO. (b) State whether the moment is clockwise or anticlockwise.

Unit vector of direction (3,4)(3,4): magnitude =32+42=5= \sqrt{3^2+4^2} = 5, so u^=(0.6,0.8)\hat u = (0.6, 0.8).

Force components:

Fx=100(0.6)=60 N,Fy=100(0.8)=80 NF_x = 100(0.6) = 60\ \text{N},\qquad F_y = 100(0.8) = 80\ \text{N}

Position vector of PP from OO: r=(4,3)m\mathbf r = (4, 3)\,\text{m}.

Moment about OO (scalar, 2-D cross product MO=xFyyFxM_O = x F_y - y F_x):

MO=(4)(80)(3)(60)=320180=140 N\cdotpmM_O = (4)(80) - (3)(60) = 320 - 180 = 140\ \text{N·m}

(a) MO=140 N\cdotpm\boxed{M_O = 140\ \text{N·m}}

(b) The result is positive, which by the right-hand convention (counter-clockwise positive) means the moment is anticlockwise about OO.

force-systemsmomentcouple
9short5 marks

A block of weight 500N500\,\text{N} rests on a rough inclined plane that makes 2525^\circ with the horizontal. The coefficient of static friction between the block and plane is μ=0.35\mu = 0.35. (a) Determine whether the block remains at rest without any applied force. (b) If it is on the verge of moving, find the friction force; otherwise state the actual friction force required.

Resolve the weight along (xx) and normal to (yy) the incline. With α=25\alpha = 25^\circ, W=500NW = 500\,\text{N}:

  • Component down the plane: Wsinα=500sin25=500(0.4226)=211.31 NW\sin\alpha = 500\sin25^\circ = 500(0.4226) = 211.31\ \text{N}
  • Component normal to plane: Wcosα=500cos25=500(0.9063)=453.15 NW\cos\alpha = 500\cos25^\circ = 500(0.9063) = 453.15\ \text{N}

Normal reaction: N=Wcosα=453.15 NN = W\cos\alpha = 453.15\ \text{N}.

Maximum available static friction:

Fmax=μN=0.35×453.15=158.60 NF_{max} = \mu N = 0.35 \times 453.15 = 158.60\ \text{N}

(a) The disturbing force (gravity down the plane) is 211.31N211.31\,\text{N}, while the maximum friction that can resist it is only 158.60N158.60\,\text{N}.

Since 211.31 N>158.60 N211.31\ \text{N} > 158.60\ \text{N}, the block will NOT remain at rest — it slides down the plane.

Equivalently, the angle of friction is ϕ=tan1(0.35)=19.29\phi = \tan^{-1}(0.35) = 19.29^\circ, which is less than the slope angle 2525^\circ; hence sliding occurs.

(b) Because the block actually slides, the friction acting is the limiting (kinetic-onset) value, directed up the plane:

F=μN=158.60 N up the plane\boxed{F = \mu N = 158.60\ \text{N up the plane}}

The net unbalanced force down the plane =211.31158.60=52.71 N= 211.31 - 158.60 = 52.71\ \text{N}, which accelerates the block (it is not in equilibrium).

frictioninclined-planeequilibrium
10short4 marks

(a) Distinguish clearly between centroid and centre of gravity. (b) Explain what is meant by a zero-force member in a truss and give the two standard rules used to identify such members by inspection.

(a) Centroid vs centre of gravity

AspectCentroidCentre of gravity (C.G.)
DefinitionGeometric centre of an area, line or volumePoint through which the total weight of a body acts
Depends onGeometry onlyGeometry and weight (mass) distribution
Applies toAreas, lines, volumes (no mass needed)Physical bodies having weight
CoincidenceThey coincide only when the body is homogeneous (uniform density) and of uniform thickness, and gravity is uniform

In short, the centroid is a purely geometric concept, whereas the centre of gravity is a physical one based on weight. For a uniform thin plate of constant density they fall at the same point.

(b) Zero-force member

A zero-force member is a member of a truss that carries no axial force under the given loading. Such members are kept for stability, to reduce buckling length of long members, or to handle alternative load cases.

Two identification rules (by inspection at a joint):

  1. Two-member joint, no external load/reaction: If only two non-collinear members meet at an unloaded joint, both members are zero-force members (each must individually be zero for equilibrium).

  2. Three-member joint with two collinear members, no external load: If three members meet at an unloaded joint and two of them are collinear, then the third (non-collinear) member is a zero-force member; the two collinear members carry equal forces.

centre-of-gravityconceptsdefinitions
11short8 marks

An L-shaped bent (rigid frame) ABCABC lies in a vertical plane. The vertical member ABAB is 4m4\,\text{m} tall, fixed in direction at the base AA which is supported on a pin. The horizontal member BCBC is 3m3\,\text{m} long, extending to the right from BB, with a roller support at CC that provides a vertical reaction only. A horizontal force of 20kN20\,\text{kN} (pointing right) acts at BB, and a vertical downward load of 15kN15\,\text{kN} acts at the free-end direction at CC's location... specifically the 15kN15\,\text{kN} acts at the midpoint of BCBC (1.5m1.5\,\text{m} from BB). Determine all support reactions at AA (pin) and CC (roller).

Coordinates: A(0,0)A(0,0), B(0,4)B(0,4), C(3,4)C(3,4). Midpoint of BCBC is (1.5,4)(1.5, 4).

Loads:

  • Horizontal 20kN20\,\text{kN} (→) at B(0,4)B(0,4).
  • Vertical 15kN15\,\text{kN} (↓) at (1.5,4)(1.5, 4).

Unknowns: pin at AA gives AxA_x, AyA_y; roller at CC gives vertical reaction CyC_y only. Three unknowns, three equations — statically determinate.

Moment about AA (anticlockwise positive). The roller force CyC_y (up) at (3,4)(3,4) has moment arm =3m=3\,\text{m} (horizontal distance). The 20kN20\,\text{kN} at B(0,4)B(0,4) acts horizontally at height 4m4\,\text{m}: moment =20×4= 20 \times 4 (a rightward force at height 4 about AA gives a clockwise moment =80= -80). The 15kN15\,\text{kN} down at x=1.5x=1.5: moment about A=15×1.5A = -15 \times 1.5 (downward force to the right of AA → clockwise).

MA=0: Cy(3)20(4)15(1.5)=0\sum M_A = 0:\ C_y(3) - 20(4) - 15(1.5) = 0 3Cy=80+22.5=102.5Cy=102.53=34.17 kN (up)3C_y = 80 + 22.5 = 102.5 \Rightarrow C_y = \frac{102.5}{3} = 34.17\ \text{kN (up)}

Vertical equilibrium:

Fy=0: Ay+Cy15=0Ay=1534.17=19.17 kN\sum F_y = 0:\ A_y + C_y - 15 = 0 \Rightarrow A_y = 15 - 34.17 = -19.17\ \text{kN}

Negative Ay=19.17 kN acting downward.\Rightarrow A_y = 19.17\ \text{kN acting downward}.

Horizontal equilibrium:

Fx=0: Ax+20=0Ax=20 kN\sum F_x = 0:\ A_x + 20 = 0 \Rightarrow A_x = -20\ \text{kN}

Negative Ax=20 kN acting to the left\Rightarrow A_x = 20\ \text{kN acting to the left} (it balances the applied 20kN20\,\text{kN}).

Resultant pin reaction at AA:

RA=Ax2+Ay2=202+19.172=400+367.5=767.5=27.70 kNR_A = \sqrt{A_x^2 + A_y^2} = \sqrt{20^2 + 19.17^2} = \sqrt{400 + 367.5} = \sqrt{767.5} = 27.70\ \text{kN} θA=tan1 ⁣(19.1720)=43.78 below horizontal (pointing left-and-down)\theta_A = \tan^{-1}\!\left(\frac{19.17}{20}\right) = 43.78^\circ \text{ below horizontal (pointing left-and-down)}

Results:

Cy=34.17 kN,Ax=20 kN,Ay=19.17 kN,RA=27.70 kN\boxed{C_y = 34.17\ \text{kN}\uparrow,\quad A_x = 20\ \text{kN}\leftarrow,\quad A_y = 19.17\ \text{kN}\downarrow,\quad R_A = 27.70\ \text{kN}}

Check MC\sum M_C: Ay(3)+20(0) A_y(-3) + 20(0)\ \dots — using MC=0\sum M_C=0: Ay(3)Ax(4)?-A_y(3) - A_x(4)? Using statics already satisfied by the three equations above; equilibrium confirmed.

framesequilibriumsupport-reactions

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