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Section A: Long Answer Questions

Attempt all questions.

5 questions
1long8 marks

Derive the Newton-Raphson iteration formula from the Taylor series expansion and state its order of convergence. In a civil-engineering design problem the depth of flow xx (in metres) satisfies the cubic equation

f(x)=x3+2x2+10x20=0.f(x) = x^3 + 2x^2 + 10x - 20 = 0.

Using the Newton-Raphson method with the initial guess x0=1x_0 = 1, perform iterations until two successive approximations agree to four decimal places. Show every iteration in a table.

Derivation. Let xnx_n be an approximation to a root α\alpha of f(x)=0f(x)=0. Expand ff in a Taylor series about xnx_n and retain terms up to first order:

f(xn+1)f(xn)+(xn+1xn)f(xn).f(x_{n+1}) \approx f(x_n) + (x_{n+1}-x_n)\,f'(x_n).

Setting f(xn+1)=0f(x_{n+1})=0 and solving for xn+1x_{n+1} gives the Newton-Raphson formula

xn+1=xnf(xn)f(xn),f(xn)0.\boxed{\,x_{n+1} = x_n - \dfrac{f(x_n)}{f'(x_n)}\,},\qquad f'(x_n)\neq 0.

Order of convergence. If α\alpha is a simple root, the error en+1f(α)2f(α)en2e_{n+1} \approx \dfrac{f''(\alpha)}{2f'(\alpha)}e_n^{2}, so convergence is quadratic (order 2).

Application. Here

f(x)=x3+2x2+10x20,f(x)=3x2+4x+10.f(x) = x^3 + 2x^2 + 10x - 20, \qquad f'(x) = 3x^2 + 4x + 10.

Iteration table (working to 6 d.p.):

nnxnx_nf(xn)f(x_n)f(xn)f'(x_n)xn+1=xnf/fx_{n+1}=x_n-f/f'
01.000000-7.00000017.0000001.411765
11.4117650.91756621.6262981.369336
21.3693360.01114821.1025931.368808
31.3688080.00000221.0961401.368808

Since x3x_3 and x4x_4 agree to four decimal places (1.36881.3688), the iteration is stopped.

Root:   x1.3688 m\;\boxed{x \approx 1.3688\ \text{m}} (check: f(1.3688)2×1060f(1.3688) \approx 2\times10^{-6} \approx 0).

roots-of-equationsnewton-raphsonconvergence
2long8 marks

Construct the Newton's divided-difference interpolating polynomial for the following (unequally spaced) field-survey data, where xx is a horizontal distance (m) and yy a measured ground reduced level (m):

xx1247
yy151750

Hence estimate the reduced level at x=3mx = 3\,\text{m} and at x=5mx = 5\,\text{m}.

Divided-difference table. With f[xi,]f[x_i,\dots] denoting divided differences:

xxyy1st DD2nd DD3rd DD
11
5121=4\frac{5-1}{2-1}=4
256441=0.66667\frac{6-4}{4-1}=0.66667
17542=6\frac{17-5}{4-2}=610.6666771=0.05556\frac{1-0.66667}{7-1}=0.05556
41711672=1.0\frac{11-6}{7-2}=1.0
501774=11\frac{50-17}{7-4}=11
750

Newton's divided-difference polynomial (using the leading entries):

P(x)=1+4(x1)+0.66667(x1)(x2)+0.05556(x1)(x2)(x4).P(x) = 1 + 4(x-1) + 0.66667(x-1)(x-2) + 0.05556(x-1)(x-2)(x-4).

Estimate at x=3x=3:

P(3)=1+4(2)+0.66667(2)(1)+0.05556(2)(1)(1)P(3) = 1 + 4(2) + 0.66667(2)(1) + 0.05556(2)(1)(-1) =1+8+1.333330.11111=10.2222 m.= 1 + 8 + 1.33333 - 0.11111 = \boxed{10.2222\ \text{m}}.

Estimate at x=5x=5:

P(5)=1+4(4)+0.66667(4)(3)+0.05556(4)(3)(1)P(5) = 1 + 4(4) + 0.66667(4)(3) + 0.05556(4)(3)(1) =1+16+8.00000+0.66667=25.6667 m.= 1 + 16 + 8.00000 + 0.66667 = \boxed{25.6667\ \text{m}}.

Thus the interpolated reduced levels are approximately 10.22 m at x=3x=3 m and 25.67 m at x=5x=5 m.

interpolationnewton-divided-differenceextrapolation
3long8 marks

The cross-sectional discharge of a channel involves the integral

I=06dx1+x2.I = \int_{0}^{6} \frac{dx}{1+x^{2}}.

Using six equal sub-intervals (h=1h=1), evaluate II by (a) the Trapezoidal rule and (b) Simpson's 1/31/3 rule. Compare both results with the exact value tan1(6)\tan^{-1}(6) and comment on the accuracy.

Function values with f(x)=11+x2f(x)=\dfrac{1}{1+x^2}, h=1h=1:

xx0123456
f(x)f(x)1.0000000.5000000.2000000.1000000.0588240.0384620.027027

(a) Trapezoidal rule.

IT=h2[(f0+f6)+2(f1+f2+f3+f4+f5)]I_T = \frac{h}{2}\Big[(f_0+f_6) + 2(f_1+f_2+f_3+f_4+f_5)\Big] =12[1.027027+2(0.897286)]=12(2.821599)=1.410799.= \frac{1}{2}\Big[1.027027 + 2(0.897286)\Big] = \frac{1}{2}(2.821599) = \boxed{1.410799}.

(b) Simpson's 1/31/3 rule (n=6n=6, even):

IS=h3[(f0+f6)+4(f1+f3+f5)+2(f2+f4)]I_S = \frac{h}{3}\Big[(f_0+f_6) + 4(f_1+f_3+f_5) + 2(f_2+f_4)\Big] =13[1.027027+4(0.638462)+2(0.258824)]= \frac{1}{3}\Big[1.027027 + 4(0.638462) + 2(0.258824)\Big] =13[1.027027+2.553846+0.517647]=13(4.098520)=1.366173.= \frac{1}{3}\Big[1.027027 + 2.553846 + 0.517647\Big] = \frac{1}{3}(4.098520) = \boxed{1.366173}.

Comparison. Exact value =tan1(6)=1.405648= \tan^{-1}(6) = 1.405648.

MethodEstimateAbsolute error
Trapezoidal1.4107990.005151
Simpson 1/31.3661730.039475

Comment. Simpson's rule is normally more accurate (error O(h4)O(h^4) versus O(h2)O(h^2)). Here the integrand is sharply peaked near x=0x=0 where the curvature is large, so with the coarse spacing h=1h=1 the trapezoidal estimate happens to be numerically closer to the exact value. Reducing hh (more sub-intervals) makes Simpson's rule converge faster and clearly outperform the trapezoidal rule.

numerical-integrationtrapezoidal-rulesimpson-rule
4long8 marks

State the condition (diagonal dominance) under which the Gauss-Seidel iterative method is guaranteed to converge. Solve the following system of equations by the Gauss-Seidel method, starting from (x,y,z)=(0,0,0)(x,y,z)=(0,0,0) and iterating until each unknown is correct to three decimal places:

20x+y2z=17,3x+20yz=18,2x3y+20z=25.\begin{aligned} 20x + y - 2z &= 17,\\ 3x + 20y - z &= -18,\\ 2x - 3y + 20z &= 25. \end{aligned}

Convergence condition. Gauss-Seidel converges (for any starting vector) if the coefficient matrix is strictly diagonally dominant, i.e. for each row ii

aii>jiaij.|a_{ii}| > \sum_{j\neq i} |a_{ij}|.

Check: Row 1: 20>1+2=320 > 1+2=3 ✓; Row 2: 20>3+1=420 > 3+1=4 ✓; Row 3: 20>2+3=520 > 2+3=5 ✓. The system is diagonally dominant, so convergence is guaranteed.

Iteration formulae (solve each equation for its diagonal unknown):

x=17y+2z20,y=183x+z20,z=252x+3y20.x = \frac{17 - y + 2z}{20},\quad y = \frac{-18 - 3x + z}{20},\quad z = \frac{25 - 2x + 3y}{20}.

Using the latest available values within each sweep:

Iterxxyyzz
10.850000-1.0275001.010875
21.002463-0.9998260.999780
30.999969-1.0000061.000002
41.000001-1.0000001.000000

From iteration 3 onwards the values are stable to three decimal places.

Solution:   x=1.000,  y=1.000,  z=1.000\;\boxed{x = 1.000,\; y = -1.000,\; z = 1.000} (verifies all three original equations exactly).

linear-systemsgauss-seideliterative-methods
5long8 marks

Write down the fourth-order Runge-Kutta (RK4) formula for the initial value problem dydx=f(x,y), y(x0)=y0\dfrac{dy}{dx}=f(x,y),\ y(x_0)=y_0. The vertical motion of a settling particle is modelled by

dydx=x+y,y(0)=1.\frac{dy}{dx} = x + y, \qquad y(0) = 1.

Using RK4 with step size h=0.1h = 0.1, compute y(0.1)y(0.1) and y(0.2)y(0.2). Compare y(0.2)y(0.2) with the exact solution y=2exx1y = 2e^{x} - x - 1.

RK4 formula. For each step,

k1=hf(xn,yn),k2=hf ⁣(xn+h2,yn+k12),k_1 = h\,f(x_n,y_n),\quad k_2 = h\,f\!\left(x_n+\tfrac{h}{2},\,y_n+\tfrac{k_1}{2}\right), k3=hf ⁣(xn+h2,yn+k22),k4=hf(xn+h,yn+k3),k_3 = h\,f\!\left(x_n+\tfrac{h}{2},\,y_n+\tfrac{k_2}{2}\right),\quad k_4 = h\,f(x_n+h,\,y_n+k_3), yn+1=yn+16(k1+2k2+2k3+k4).y_{n+1} = y_n + \tfrac{1}{6}\left(k_1 + 2k_2 + 2k_3 + k_4\right).

Here f(x,y)=x+yf(x,y)=x+y, h=0.1h=0.1. (Below the kk values are written as ff-evaluations; multiply by hh in the weighted sum.)

Step 1: x0=0, y0=1y(0.1)x_0=0,\ y_0=1 \Rightarrow y(0.1)

k1=f(0,1)=1.000000k_1=f(0,1)=1.000000 k2=f(0.05,1+0.051)=f(0.05,1.05)=1.100000k_2=f(0.05,\,1+0.05\cdot1)=f(0.05,1.05)=1.100000 k3=f(0.05,1+0.051.1)=f(0.05,1.055)=1.105000k_3=f(0.05,\,1+0.05\cdot1.1)=f(0.05,1.055)=1.105000 k4=f(0.1,1+0.11.105)=f(0.1,1.1105)=1.210500k_4=f(0.1,\,1+0.1\cdot1.105)=f(0.1,1.1105)=1.210500 y(0.1)=1+0.16(1+2(1.1)+2(1.105)+1.2105)=1+0.16(6.620500)=1.110342.y(0.1)=1+\tfrac{0.1}{6}\big(1+2(1.1)+2(1.105)+1.2105\big)=1+\tfrac{0.1}{6}(6.620500)=\boxed{1.110342}.

Step 2: x1=0.1, y1=1.110342y(0.2)x_1=0.1,\ y_1=1.110342 \Rightarrow y(0.2)

k1=f(0.1,1.110342)=1.210342k_1=f(0.1,1.110342)=1.210342 k2=f(0.15,1.110342+0.051.210342)=f(0.15,1.170859)=1.320859k_2=f(0.15,\,1.110342+0.05\cdot1.210342)=f(0.15,1.170859)=1.320859 k3=f(0.15,1.110342+0.051.320859)=f(0.15,1.176385)=1.326385k_3=f(0.15,\,1.110342+0.05\cdot1.320859)=f(0.15,1.176385)=1.326385 k4=f(0.2,1.110342+0.11.326385)=f(0.2,1.242980)=1.442980k_4=f(0.2,\,1.110342+0.1\cdot1.326385)=f(0.2,1.242980)=1.442980 y(0.2)=1.110342+0.16(1.210342+2(1.320859)+2(1.326385)+1.442980)y(0.2)=1.110342+\tfrac{0.1}{6}\big(1.210342+2(1.320859)+2(1.326385)+1.442980\big) =1.110342+0.16(7.947810)=1.242805.=1.110342+\tfrac{0.1}{6}(7.947810)=\boxed{1.242805}.

Comparison. Exact: y(0.2)=2e0.20.21=1.242806y(0.2)=2e^{0.2}-0.2-1=1.242806. The RK4 estimate 1.2428051.242805 differs by only 1×106\approx 1\times10^{-6}, confirming the high (fourth-order) accuracy of the method.

ordinary-differential-equationsrunge-kuttainitial-value-problem
B

Section B: Short Answer Questions

Attempt all questions.

6 questions
6short8 marks

Solve the following system of linear equations by Gauss elimination with back-substitution:

2x+y+z=10,3x+2y+3z=18,x+4y+9z=16.\begin{aligned} 2x + y + z &= 10,\\ 3x + 2y + 3z &= 18,\\ x + 4y + 9z &= 16. \end{aligned}

Augmented matrix:

[211103231814916].\left[\begin{array}{ccc|c} 2 & 1 & 1 & 10 \\ 3 & 2 & 3 & 18 \\ 1 & 4 & 9 & 16 \end{array}\right].

Step 1 — eliminate xx from rows 2 and 3 (pivot a11=2a_{11}=2): R2R232R1R_2 \leftarrow R_2 - \tfrac{3}{2}R_1 and R3R312R1R_3 \leftarrow R_3 - \tfrac{1}{2}R_1:

[2111000.51.5303.58.511].\left[\begin{array}{ccc|c} 2 & 1 & 1 & 10 \\ 0 & 0.5 & 1.5 & 3 \\ 0 & 3.5 & 8.5 & 11 \end{array}\right].

Step 2 — eliminate yy from row 3 (pivot a22=0.5a_{22}=0.5): R3R33.50.5R2=R37R2R_3 \leftarrow R_3 - \tfrac{3.5}{0.5}R_2 = R_3 - 7R_2:

[2111000.51.5300210].\left[\begin{array}{ccc|c} 2 & 1 & 1 & 10 \\ 0 & 0.5 & 1.5 & 3 \\ 0 & 0 & -2 & -10 \end{array}\right].

Back-substitution.

z=102=5.z = \frac{-10}{-2} = 5. 0.5y+1.5(5)=3    0.5y=37.5=4.5    y=9.0.5y + 1.5(5) = 3 \;\Rightarrow\; 0.5y = 3 - 7.5 = -4.5 \;\Rightarrow\; y = -9. 2x+(9)+5=10    2x=14    x=7.2x + (-9) + 5 = 10 \;\Rightarrow\; 2x = 14 \;\Rightarrow\; x = 7.

Solution:   x=7,  y=9,  z=5\;\boxed{x = 7,\; y = -9,\; z = 5} (check in eqn 3: 7+4(9)+9(5)=736+45=167 + 4(-9) + 9(5) = 7 - 36 + 45 = 16 ✓).

linear-systemsgauss-eliminationback-substitution
7short8 marks

The following table gives equally spaced data with step h=1h=1:

xx0123
yy12928

Construct the forward-difference table and use Newton's forward interpolation formula to estimate yy at x=1.5x = 1.5.

Forward-difference table (Δky\Delta^k y):

xxyyΔy\Delta yΔ2y\Delta^2 yΔ3y\Delta^3 y
01
1
126
76
2912
19
328

Leading differences: y0=1, Δy0=1, Δ2y0=6, Δ3y0=6y_0=1,\ \Delta y_0=1,\ \Delta^2 y_0=6,\ \Delta^3 y_0=6.

Newton's forward formula with p=xx0h=1.501=1.5p=\dfrac{x-x_0}{h}=\dfrac{1.5-0}{1}=1.5:

y=y0+pΔy0+p(p1)2!Δ2y0+p(p1)(p2)3!Δ3y0.y = y_0 + p\,\Delta y_0 + \frac{p(p-1)}{2!}\Delta^2 y_0 + \frac{p(p-1)(p-2)}{3!}\Delta^3 y_0.

Compute each term:

  • y0=1y_0 = 1
  • pΔy0=1.5(1)=1.5p\,\Delta y_0 = 1.5(1) = 1.5
  • 1.5(0.5)2(6)=0.752(6)=0.375×6=2.25\dfrac{1.5(0.5)}{2}(6) = \dfrac{0.75}{2}(6) = 0.375\times6 = 2.25
  • 1.5(0.5)(0.5)6(6)=0.3756(6)=0.375\dfrac{1.5(0.5)(-0.5)}{6}(6) = \dfrac{-0.375}{6}(6) = -0.375
y(1.5)=1+1.5+2.250.375=4.375.y(1.5) = 1 + 1.5 + 2.25 - 0.375 = \boxed{4.375}.

(The data correspond to y=x3+1y=x^3+1; exact 1.53+1=4.3751.5^3+1=4.375, confirming the result.)

interpolationnewton-forward-differencefinite-differences
8short8 marks

Given the tabulated values

xx12345
yy182764125

with h=1h = 1, use the forward-difference formulae to compute the first derivative dydx\dfrac{dy}{dx} and the second derivative d2ydx2\dfrac{d^2y}{dx^2} at x=1x = 1.

Forward-difference table:

xxyyΔy\Delta yΔ2y\Delta^2 yΔ3y\Delta^3 yΔ4y\Delta^4 y
11
7
2812
196
327180
376
46424
61
5125

Leading differences: Δy0=7, Δ2y0=12, Δ3y0=6, Δ4y0=0\Delta y_0=7,\ \Delta^2 y_0=12,\ \Delta^3 y_0=6,\ \Delta^4 y_0=0.

First derivative at x=1x=1 (start of table, forward formula):

dydxx0=1h(Δy0Δ2y02+Δ3y03Δ4y04)\left.\frac{dy}{dx}\right|_{x_0} = \frac{1}{h}\left(\Delta y_0 - \frac{\Delta^2 y_0}{2} + \frac{\Delta^3 y_0}{3} - \frac{\Delta^4 y_0}{4}\right) =11(7122+6304)=76+20=3.= \frac{1}{1}\left(7 - \frac{12}{2} + \frac{6}{3} - \frac{0}{4}\right) = 7 - 6 + 2 - 0 = \boxed{3}.

Second derivative at x=1x=1:

d2ydx2x0=1h2(Δ2y0Δ3y0+1112Δ4y0)\left.\frac{d^2y}{dx^2}\right|_{x_0} = \frac{1}{h^2}\left(\Delta^2 y_0 - \Delta^3 y_0 + \frac{11}{12}\Delta^4 y_0\right) =11(126+11120)=6.= \frac{1}{1}\left(12 - 6 + \frac{11}{12}\cdot 0\right) = \boxed{6}.

The data follow y=x3y=x^3, for which y(1)=3x2=3y'(1)=3x^2=3 and y(1)=6x=6y''(1)=6x=6 — the numerical results match exactly.

numerical-differentiationfinite-differencesderivatives
9short4 marks

Using the Bisection method, find an approximation to 10\sqrt{10} by locating the positive root of f(x)=x210=0f(x) = x^2 - 10 = 0 in the interval [3,4][3, 4]. Perform five iterations and state the approximate root.

Since f(3)=910=1<0f(3) = 9-10 = -1 < 0 and f(4)=1610=6>0f(4) = 16-10 = 6 > 0, a root lies in [3,4][3,4]. At each step take c=a+b2c=\frac{a+b}{2} and keep the half-interval where the sign of ff changes.

Iteraabbc=a+b2c=\frac{a+b}{2}f(c)f(c)New interval
13.00004.00003.5000+2.2500[3.0000,3.5000][3.0000,3.5000]
23.00003.50003.2500+0.5625[3.0000,3.2500][3.0000,3.2500]
33.00003.25003.1250-0.2344[3.1250,3.2500][3.1250,3.2500]
43.12503.25003.1875+0.1602[3.1250,3.1875][3.1250,3.1875]
53.12503.18753.1563-0.0381[3.1563,3.1875][3.1563,3.1875]

After five iterations the root is bracketed in [3.1563,3.1875][3.1563, 3.1875].

Approximate root:   x3.1563\;\boxed{x \approx 3.1563} (true value 10=3.16228\sqrt{10}=3.16228; error <0.007<0.007).

roots-of-equationsbisection-method
10short4 marks

Using Euler's method with step size h=0.1h = 0.1, solve dydx=x+y\dfrac{dy}{dx} = x + y with y(0)=1y(0) = 1, and find y(0.3)y(0.3).

Euler's formula: yn+1=yn+hf(xn,yn)y_{n+1} = y_n + h\,f(x_n, y_n), with f(x,y)=x+yf(x,y)=x+y, h=0.1h=0.1.

Stepxnx_nyny_nf(xn,yn)=xn+ynf(x_n,y_n)=x_n+y_nyn+1=yn+hfy_{n+1}=y_n+h f
10.01.0000001.0000001.100000
20.11.1000001.2000001.220000
30.21.2200001.4200001.362000

Result:   y(0.3)1.3620\;\boxed{y(0.3) \approx 1.3620}.

(The exact solution is y=2exx1y=2e^{x}-x-1, giving y(0.3)=1.39972y(0.3)=1.39972; Euler's method underestimates because it uses only the slope at the start of each interval — accuracy improves with smaller hh.)

ordinary-differential-equationseuler-method
11short8 marks

Explain how the Laplace equation 2ux2+2uy2=0\dfrac{\partial^2 u}{\partial x^2} + \dfrac{\partial^2 u}{\partial y^2} = 0 is discretized by the standard five-point finite-difference formula on a square mesh, and state the resulting (Liebmann) iteration formula. (a) A square plate is divided so that there is a single interior node whose four neighbouring boundary temperatures are 100C100^{\circ}\text{C}, 80C80^{\circ}\text{C}, 60C60^{\circ}\text{C} and 40C40^{\circ}\text{C}. Find the steady-state temperature at the interior node. (b) The same plate is now refined to give two interior nodes u1u_1 and u2u_2 in a row: u1u_1 has neighbours 100C100^{\circ}\text{C} (left), 80C80^{\circ}\text{C} (top), 60C60^{\circ}\text{C} (bottom) and u2u_2 (right); u2u_2 has neighbours u1u_1 (left), 80C80^{\circ}\text{C} (top), 60C60^{\circ}\text{C} (bottom) and 40C40^{\circ}\text{C} (right). Set up the two equations and solve for u1u_1 and u2u_2.

Discretization. On a uniform square mesh of spacing hh, replace each second derivative by a central difference:

2ux2ui+1,j2ui,j+ui1,jh2,2uy2ui,j+12ui,j+ui,j1h2.\frac{\partial^2 u}{\partial x^2} \approx \frac{u_{i+1,j} - 2u_{i,j} + u_{i-1,j}}{h^2},\qquad \frac{\partial^2 u}{\partial y^2} \approx \frac{u_{i,j+1} - 2u_{i,j} + u_{i,j-1}}{h^2}.

Substituting into Laplace's equation, the h2h^2 cancels and the five-point formula becomes

ui+1,j+ui1,j+ui,j+1+ui,j14ui,j=0,u_{i+1,j} + u_{i-1,j} + u_{i,j+1} + u_{i,j-1} - 4u_{i,j} = 0,

which rearranges to the Liebmann (Gauss-Seidel) iteration formula

ui,j=14(ui+1,j+ui1,j+ui,j+1+ui,j1).\boxed{\,u_{i,j} = \tfrac{1}{4}\big(u_{i+1,j} + u_{i-1,j} + u_{i,j+1} + u_{i,j-1}\big)\,}.

Each interior temperature equals the average of its four neighbours.

(a) Single interior node. Its four neighbours are the given boundary values 100, 80, 60, 40 C100,\ 80,\ 60,\ 40\ ^{\circ}\text{C}:

u=100+80+60+404=2804=70C.u = \frac{100 + 80 + 60 + 40}{4} = \frac{280}{4} = \boxed{70^{\circ}\text{C}}.

With only one unknown the average is exact and no iteration is needed.

(b) Two interior nodes. Apply the five-point formula at each node:

u1=100+80+60+u24=240+u24    4u1u2=240,u_1 = \frac{100 + 80 + 60 + u_2}{4} = \frac{240 + u_2}{4} \;\Rightarrow\; 4u_1 - u_2 = 240, u2=u1+80+60+404=180+u14    u1+4u2=180.u_2 = \frac{u_1 + 80 + 60 + 40}{4} = \frac{180 + u_1}{4} \;\Rightarrow\; -u_1 + 4u_2 = 180.

Solve the 2×22\times2 system. From the first, u2=4u1240u_2 = 4u_1 - 240; substitute into the second:

u1+4(4u1240)=180    15u1=1140    u1=76C.-u_1 + 4(4u_1 - 240) = 180 \;\Rightarrow\; 15u_1 = 1140 \;\Rightarrow\; u_1 = 76^{\circ}\text{C}. u2=4(76)240=64C.u_2 = 4(76) - 240 = 64^{\circ}\text{C}.

Result:   u1=76C,  u2=64C\;\boxed{u_1 = 76^{\circ}\text{C},\; u_2 = 64^{\circ}\text{C}} (a Liebmann iteration from a zero start also converges to these values).

partial-differential-equationslaplace-equationfinite-difference

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