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MATLAB Heat Transfer Simulation: Conduction, Convection & Radiation

MATLAB Heat Transfer Simulation: Conduction, Convection & Radiation

MATLAB Heat Transfer Tutorial · Conduction · Convection · Radiation · Thermal Analysis · Engineering Simulation

MATLAB heat transfer simulation is a useful way for engineering students to move from equations on paper to a numerical model they can inspect, modify and validate. In this tutorial, we build a practical steady-state thermal model covering conduction, convection and radiation. The complete MATLAB script calculates the three modes, solves a combined wall problem, produces seven engineering plots and checks the final energy balance.

The example is deliberately small enough to understand without a large CFD package, but it still introduces professional numerical habits: clear inputs, SI-unit consistency, a nonlinear energy balance, numerical root solving, parameter sensitivity and validation. You can run the supplied .m file first and then change the inputs to turn the article into a hands-on laboratory exercise.

Conduction + Convection + Radiation in One MATLAB Model

The model represents a hot fluid, an inner convection boundary, a solid wall and an outer surface that loses heat through both convection and thermal radiation. Seven MATLAB figures are generated automatically.

1. Introduction to Heat Transfer

Heat transfer is the movement of thermal energy caused by a temperature difference. Mechanical, chemical, aerospace, energy and HVAC systems repeatedly use the same three mechanisms: conduction through matter, convection between a surface and a fluid, and thermal radiation between surfaces or surroundings.

Real systems often involve more than one mechanism at the same time. A wall separating a hot space from a colder environment may receive heat from the indoor air by convection, conduct it through the solid and then reject it outdoors by both convection and radiation. A calculation that considers only one mechanism can therefore miss part of the physical heat balance.

MATLAB is useful because it turns these relationships into a repeatable numerical experiment. Once the base case works, a few input changes can show how wall thickness, thermal conductivity, convection coefficient and emissivity affect the result.

Learning approach: don't treat the script as a black box. First identify the physical path of heat, then identify the equation for each part, then follow how MATLAB converts those equations into a numerical solution.

2. Learning Objectives

After completing this tutorial, students should be able to:

  • distinguish conduction, convection and radiation in a thermal system;
  • apply Fourier law, Newton's law of cooling and the Stefan-Boltzmann relation;
  • build a simple thermal-resistance model in MATLAB;
  • solve a nonlinear surface-temperature balance using fzero;
  • generate engineering plots from calculated variables;
  • study the effects of convection coefficient, emissivity and wall thickness;
  • check whether a numerical solution satisfies an energy balance.

3. Three Modes of Heat Transfer

ModeMain relationshipPhysical meaningImportant parameters
ConductionQ = kA(T1 - T2)/LEnergy transfer through a material because of a temperature gradient.k, A, L, temperature difference
ConvectionQ = hA(Ts - T)Heat exchange between a surface and a surrounding fluid.h, A, surface temperature, fluid temperature
RadiationQ = εσA(Ts4 - Tsur4)Thermal energy exchanged through electromagnetic radiation.ε, σ, A, absolute temperatures

Conduction is controlled by material conductivity and the temperature gradient. Convection introduces the heat-transfer coefficient h. Radiation is different because temperature appears to the fourth power and the equation requires absolute temperature.

4. Governing Equations

Fourier law for conduction

Qcond = kA(T1 - T2) / L

For the plane wall, k is thermal conductivity, A is area and L is wall thickness. Increasing k increases heat transfer, while increasing L increases conduction resistance.

Newton's law of cooling

Qconv = hA(Ts - T)

The coefficient h depends on fluid and flow conditions. In a detailed study it may come from Reynolds, Prandtl and Nusselt correlations. Here it is an input so students can focus on the thermal model.

Stefan-Boltzmann radiation

Qrad = εσA(Ts4 - Tsur4)

The emissivity ε is dimensionless and σ is the Stefan-Boltzmann constant. Both temperatures in the fourth-power expression are absolute temperatures in Kelvin.

Combined steady-state balance

Qcond = Qconv,out + Qrad

At steady state, heat reaching the outer surface equals heat leaving it. Radiation makes the equation nonlinear, so the unknown outer surface temperature is solved numerically.

5. MATLAB Problem Definition

The base case represents a one-square-metre wall with thickness 0.10 m and thermal conductivity 1.50 W/(m·K). The hot fluid is at 80°C, outdoor air is at 25°C, surroundings are at 15°C, the inner and outer convection coefficients are 12 and 10 W/(m²·K), and emissivity is 0.85.

ParameterSymbolBase valueUnit
Wall thicknessL0.10m
AreaA1.00
Thermal conductivityk1.50W/(m·K)
Hot fluid temperatureThot80°C
Inner hhin12W/(m²·K)
Outdoor fluid temperatureT25°C
Outer hhout10W/(m²·K)
Surroundings temperatureTsur15°C
Emissivityε0.85-

All calculations use SI units. That choice matters: mixed units can produce values that look reasonable while being physically wrong.

MATLAB Heat Transfer Simulation Problem


6. Complete MATLAB Code

Save the following as MATLAB_Heat_Transfer_Conduction_Convection_Radiation.m. The script calculates the base case, prints the results and creates seven MATLAB figures.

MATLAB · Complete Heat Transfer Simulation Script
%% MATLAB Heat Transfer Simulation: Conduction, Convection & Radiation
% Educational script for engineering students.
% Demonstrates conduction, convection, radiation and a combined steady
% state wall model. Uses SI units throughout.
%
% Figures generated:
% 1. Standalone conduction/convection/radiation comparison
% 2. Temperature distribution through the wall
% 3. Effect of convection coefficient h
% 4. Effect of emissivity
% 5. Radiation contribution vs emissivity
% 6. Convection vs radiation heat rejection
% 7. Effect of wall thickness

clear; clc; close all;

%% 1. INPUT PARAMETERS
L = 0.10;                 % Wall thickness [m]
A = 1.00;                 % Area [m^2]
k = 1.50;                 % Wall thermal conductivity [W/(m*K)]
T_hot = 80;               % Hot fluid temperature [deg C]
h_in = 12;                % Inner convection coefficient [W/(m^2*K)]
T_inf = 25;               % Outdoor fluid temperature [deg C]
h_out = 10;               % Outer convection coefficient [W/(m^2*K)]
T_sur = 15;               % Radiation surroundings temperature [deg C]
epsilon = 0.85;           % Surface emissivity [-]
sigma = 5.670374419e-8;   % Stefan-Boltzmann constant [W/(m^2*K^4)]

%% 2. STANDALONE CONDUCTION EXAMPLE
% Fourier law: Q = k*A*(T1-T2)/L
T1 = 80; T2 = 25;
Q_conduction = k*A*(T1-T2)/L;

%% 3. STANDALONE CONVECTION EXAMPLE
% Newton cooling: Q = h*A*(Ts-T_inf)
Ts_conv = 60;
Q_convection = h_out*A*(Ts_conv-T_inf);

%% 4. STANDALONE RADIATION EXAMPLE
% Stefan-Boltzmann: Q = eps*sigma*A*(Ts^4-Tsur^4)
Ts_rad = 60 + 273.15;
Tsur_K = T_sur + 273.15;
Q_radiation = epsilon*sigma*A*(Ts_rad^4-Tsur_K^4);

%% 5. COMBINED STEADY-STATE MODEL
% Hot fluid -> inner convection -> wall conduction -> outer surface
% Outer surface rejects heat by BOTH convection and radiation.
%
% At steady state:
% Q_cond = Q_conv,out + Q_rad
%
% Inner convection + wall conduction are represented by resistances.
R_in = 1/(h_in*A);        % [K/W]
R_cond = L/(k*A);         % [K/W]

% Heat arriving at outer surface for an assumed outer surface temperature.
Q_to_surface = @(Ts_C) (T_hot-Ts_C)/(R_in+R_cond);

% Heat leaving outer surface by convection + radiation.
Q_from_surface = @(Ts_C) h_out*A*(Ts_C-T_inf) + ...
    epsilon*sigma*A*((Ts_C+273.15)^4-(T_sur+273.15)^4);

% Solve nonlinear surface energy balance.
balance = @(Ts_C) Q_to_surface(Ts_C)-Q_from_surface(Ts_C);
Ts_out = fzero(balance,35);

% Final combined-model results.
Q_total = Q_to_surface(Ts_out);
Q_conv_out = h_out*A*(Ts_out-T_inf);
Q_rad_out = epsilon*sigma*A*((Ts_out+273.15)^4-(T_sur+273.15)^4);
Ts_in = T_hot-Q_total*R_in;
q_total = Q_total/A;
balance_error = Q_total-(Q_conv_out+Q_rad_out);
conv_fraction = 100*Q_conv_out/Q_total;
rad_fraction = 100*Q_rad_out/Q_total;

%% 6. PRINT RESULTS
fprintf('\n============================================================\n');
fprintf(' MATLAB HEAT TRANSFER SIMULATION\n');
fprintf(' Conduction + Convection + Radiation\n');
fprintf('============================================================\n');
fprintf('\nINPUTS\n');
fprintf('Wall thickness            = %.4f m\n',L);
fprintf('Thermal conductivity      = %.3f W/(m K)\n',k);
fprintf('Area                      = %.3f m^2\n',A);
fprintf('Hot fluid temperature     = %.2f deg C\n',T_hot);
fprintf('Outdoor fluid temperature = %.2f deg C\n',T_inf);
fprintf('Surroundings temperature  = %.2f deg C\n',T_sur);
fprintf('Inner h                   = %.2f W/(m^2 K)\n',h_in);
fprintf('Outer h                   = %.2f W/(m^2 K)\n',h_out);
fprintf('Emissivity                = %.3f\n',epsilon);
fprintf('\nCOMBINED MODEL RESULTS\n');
fprintf('Inner wall surface temp   = %.3f deg C\n',Ts_in);
fprintf('Outer wall surface temp   = %.3f deg C\n',Ts_out);
fprintf('Total heat transfer       = %.3f W\n',Q_total);
fprintf('Heat flux                 = %.3f W/m^2\n',q_total);
fprintf('Outer convection          = %.3f W (%.2f%%)\n',Q_conv_out,conv_fraction);
fprintf('Outer radiation           = %.3f W (%.2f%%)\n',Q_rad_out,rad_fraction);
fprintf('Energy balance error      = %.3e W\n',balance_error);
fprintf('\nSTANDALONE EXAMPLES\n');
fprintf('Conduction example        = %.3f W\n',Q_conduction);
fprintf('Convection example        = %.3f W\n',Q_convection);
fprintf('Radiation example         = %.3f W\n',Q_radiation);

%% 7. FIGURE 1 - THREE HEAT-TRANSFER MODES
figure('Name','Heat Transfer Modes','Color','w');
bar([Q_conduction,Q_convection,Q_radiation]);
grid on;
xticks(1:3); xticklabels({'Conduction','Convection','Radiation'});
ylabel('Heat-transfer rate, Q [W]');
title('Standalone Heat-Transfer Mode Comparison');
set(gca,'FontSize',11);

%% 8. FIGURE 2 - TEMPERATURE DISTRIBUTION THROUGH WALL
x = linspace(0,L,200);
T_wall = Ts_in-(Ts_in-Ts_out)*(x/L);
figure('Name','Temperature Distribution','Color','w');
plot(x,T_wall,'LineWidth',2); hold on;
plot(0,Ts_in,'o','MarkerSize',8,'LineWidth',1.5);
plot(L,Ts_out,'o','MarkerSize',8,'LineWidth',1.5);
yline(T_hot,'--','Hot fluid','LineWidth',1.2);
yline(T_inf,'--','Outdoor fluid','LineWidth',1.2);
grid on;
xlabel('Distance through wall [m]');
ylabel('Temperature [deg C]');
title('Temperature Distribution Through the Solid Wall');
legend('Wall temperature','Inner surface','Outer surface','Hot fluid','Outdoor fluid','Location','best');
set(gca,'FontSize',11);

%% 9. FIGURE 3 - CONVECTION COEFFICIENT SENSITIVITY
h_values = linspace(2,40,100);
Q_h = zeros(size(h_values));
for i = 1:numel(h_values)
    h_test = h_values(i);
    balance_h = @(Ts) Q_to_surface(Ts) - ...
        (h_test*A*(Ts-T_inf)+epsilon*sigma*A*((Ts+273.15)^4-Tsur_K^4));
    Ts_test = fzero(balance_h,35);
    Q_h(i) = Q_to_surface(Ts_test);
end
figure('Name','Convection Sensitivity','Color','w');
plot(h_values,Q_h,'LineWidth',2); grid on;
xlabel('Outer convection coefficient, h [W/(m^2 K)]');
ylabel('Total heat-transfer rate, Q [W]');
title('Effect of Convection Coefficient on Heat Transfer');
set(gca,'FontSize',11);

%% 10. FIGURE 4 - EMISSIVITY SENSITIVITY
epsilon_values = linspace(0.05,1.0,100);
Q_epsilon = zeros(size(epsilon_values));
for i = 1:numel(epsilon_values)
    eps_test = epsilon_values(i);
    balance_eps = @(Ts) Q_to_surface(Ts) - ...
        (h_out*A*(Ts-T_inf)+eps_test*sigma*A*((Ts+273.15)^4-Tsur_K^4));
    Ts_test = fzero(balance_eps,35);
    Q_epsilon(i) = Q_to_surface(Ts_test);
end
figure('Name','Radiation Sensitivity','Color','w');
plot(epsilon_values,Q_epsilon,'LineWidth',2); grid on;
xlabel('Surface emissivity, epsilon [-]');
ylabel('Total heat-transfer rate, Q [W]');
title('Effect of Surface Emissivity on Total Heat Transfer');
set(gca,'FontSize',11);

%% 11. FIGURE 5 - RADIATION CONTRIBUTION VS EMISSIVITY
radiation_fraction = zeros(size(epsilon_values));
for i = 1:numel(epsilon_values)
    eps_test = epsilon_values(i);
    balance_eps = @(Ts) Q_to_surface(Ts) - ...
        (h_out*A*(Ts-T_inf)+eps_test*sigma*A*((Ts+273.15)^4-Tsur_K^4));
    Ts_test = fzero(balance_eps,35);
    Q_test = Q_to_surface(Ts_test);
    Q_rad_test = eps_test*sigma*A*((Ts_test+273.15)^4-Tsur_K^4);
    radiation_fraction(i) = 100*Q_rad_test/Q_test;
end
figure('Name','Radiation Contribution','Color','w');
plot(epsilon_values,radiation_fraction,'LineWidth',2); grid on;
xlabel('Surface emissivity, epsilon [-]');
ylabel('Radiation contribution [%]');
title('Radiation Contribution to Total Heat Rejection');
set(gca,'FontSize',11);

%% 12. FIGURE 6 - OUTER-SURFACE HEAT REJECTION
figure('Name','Heat Rejection Contribution','Color','w');
bar([Q_conv_out,Q_rad_out]); grid on;
xticks(1:2); xticklabels({'Convection','Radiation'});
ylabel('Heat-transfer rate [W]');
title('Outer-Surface Heat Rejection Mechanisms');
set(gca,'FontSize',11);

%% 13. FIGURE 7 - WALL THICKNESS SENSITIVITY
L_values = linspace(0.01,0.30,100);
Q_L = zeros(size(L_values));
for i = 1:numel(L_values)
    L_test = L_values(i);
    R_cond_test = L_test/(k*A);
    Q_surface_test = @(Ts) (T_hot-Ts)/(R_in+R_cond_test);
    balance_L = @(Ts) Q_surface_test(Ts) - ...
        (h_out*A*(Ts-T_inf)+epsilon*sigma*A*((Ts+273.15)^4-Tsur_K^4));
    Ts_test = fzero(balance_L,35);
    Q_L(i) = Q_surface_test(Ts_test);
end
figure('Name','Wall Thickness Sensitivity','Color','w');
plot(L_values,Q_L,'LineWidth',2); grid on;
xlabel('Wall thickness, L [m]');
ylabel('Total heat-transfer rate, Q [W]');
title('Effect of Wall Thickness on Heat Transfer');
set(gca,'FontSize',11);

%% 14. EDUCATIONAL SUMMARY
fprintf('\n============================================================\n');
fprintf('KEY ENGINEERING OBSERVATIONS\n');
fprintf('============================================================\n');
fprintf('1. Increasing wall thickness increases conduction resistance.\n');
fprintf('2. Increasing h generally increases surface heat transfer.\n');
fprintf('3. Increasing emissivity increases radiative heat transfer.\n');
fprintf('4. Radiation uses absolute temperature and depends on T^4.\n');
fprintf('5. At steady state, heat entering equals heat leaving.\n');

%% 15. OPTIONAL REUSABLE RADIATION FUNCTION
% Example use after the script has been run:
% Q = radiationHeatTransfer(60,15,0.85,1.0)

function Q = radiationHeatTransfer(Ts_C,Tsur_C,epsilon,A)
% radiationHeatTransfer - net radiation heat transfer [W]
% Inputs: Ts_C, Tsur_C [deg C], epsilon [-], A [m^2]
    sigma = 5.670374419e-8;
    Ts_K = Ts_C + 273.15;
    Tsur_K = Tsur_C + 273.15;
    Q = epsilon*sigma*A*(Ts_K^4-Tsur_K^4);
end
How to run the MATLAB heat transfer simulation
Step 1: Define the heat-transfer problem
Set wall thickness, area, thermal conductivity, fluid temperatures, convection coefficients, emissivity and surroundings temperature.
Step 2: Calculate the individual heat-transfer modes
Use Fourier law for conduction, Newton's law of cooling for convection and the Stefan-Boltzmann relation for radiation.
Step 3: Build the combined steady-state model
Represent inner convection and wall conduction as thermal resistances and write the outer-surface balance as conduction heat in equals convection plus radiation heat out.
Step 4: Solve the nonlinear surface-temperature equation
Use MATLAB fzero to find the outer wall temperature that satisfies the combined steady-state energy balance.
Step 5: Study sensitivity and validate the result
Plot the temperature profile and sensitivity to convection coefficient, emissivity and wall thickness, then check that the energy-balance error is close to zero.

7. Explanation of the MATLAB Code

The script first clears the workspace and defines the thermal inputs. Keeping the inputs together makes the model easy to audit and modify. The next three sections calculate conduction, convection and radiation independently so students can see the individual mechanisms before studying the coupled problem.

The combined model defines R_in = 1/(h_in*A) and R_cond = L/(k*A). For an assumed outer surface temperature, MATLAB calculates the heat arriving at that surface. It separately calculates heat leaving by outdoor convection and radiation. The residual between these two quantities is passed to fzero.

When the residual reaches zero, the outer surface satisfies the steady-state energy balance. The script then calculates heat flux, convection and radiation contributions, and the balance error. The plotting sections reuse these variables for sensitivity studies rather than performing disconnected calculations.

8. Temperature Distribution Result

The wall temperature is linear in this example because the model assumes one-dimensional steady conduction, constant thermal conductivity and no internal heat generation. The plot also shows that fluid temperatures and wall-surface temperatures are not automatically the same; the difference across each fluid boundary is associated with convection.

MATLAB temperature distribution through a solid wall

Figure 2. Temperature profile through the wall, including the calculated inner and outer surface temperatures.

Use the full-size link beneath the figure when preparing a report or lecture note. The link points to the same Blogger-hosted image URL used by the displayed result.

9. Effect of Convection Coefficient

The third plot varies the outer convection coefficient from 2 to 40 W/(m²·K). For every value, MATLAB solves the surface-temperature equation again. This matters because changing h can change both the surface temperature and the final heat-transfer rate.

MATLAB heat transfer sensitivity to convection coefficient

Figure 3. Effect of the outer convection coefficient on the combined heat-transfer rate.

Student takeaway: a convection coefficient is part of a coupled boundary condition. It should not automatically be treated as a fixed heat-transfer rate multiplier when the surface temperature is unknown.

10. Effect of Emissivity

The fourth plot varies emissivity from 0.05 to 1.0. Increasing emissivity generally increases the ability of the surface to exchange thermal radiation, although the final result also depends on surface temperature and surroundings temperature.

MATLAB heat transfer sensitivity to surface emissivity

Figure 4. Effect of surface emissivity on total heat transfer.

MATLAB radiation contribution versus surface emissivity

Figure 5. Radiation contribution to total heat rejection as emissivity changes.

Important: the radiation equation uses Kelvin. The MATLAB code adds 273.15 before evaluating the fourth-power temperature terms.

11. Conduction vs Convection vs Radiation

The first plot compares the three standalone calculations. It is a teaching comparison, not a claim that the three values are independent heat losses from one identical boundary. The coupled wall model provides the physically consistent steady-state result.

MATLAB heat transfer simulation comparison of conduction convection and radiation

Figure 1. Standalone comparison of conduction, convection and radiation heat-transfer rates.

The sixth plot focuses on the actual outer-surface heat rejection in the combined model. At that surface, the incoming conduction heat is divided between convection to the outdoor fluid and radiation to the surroundings.

MATLAB convection and radiation heat rejection comparison

Figure 6. Outer-surface heat rejection split between convection and radiation.

12. Wall Thickness Sensitivity

Conduction resistance is proportional to wall thickness:

Rcond = L/(kA)

The seventh plot changes wall thickness from 0.01 to 0.30 m and resolves the coupled model at each value.

MATLAB wall thickness sensitivity heat transfer simulation

Figure 7. Effect of wall thickness on the combined steady-state heat-transfer rate.

A thicker wall generally reduces the heat-transfer rate because it increases conduction resistance. The curve is coupled to the convection and radiation boundaries, so it represents the complete model rather than conduction alone.

13. Energy-Balance Validation

A numerical result should not be accepted simply because MATLAB returns a number. The script checks:

Error = Qtotal - (Qconv,out + Qrad,out)

For a converged steady-state solution, this error should be very small relative to the heat-transfer rate. The Command Window prints the error in watts using scientific notation. The script also prints inner and outer surface temperatures, total heat transfer, heat flux and the convection/radiation contributions.

Good numerical practice: use conservation or an energy balance as a validation check whenever the governing physics provides one. A graph can look correct even when a model contains a unit or boundary-condition mistake.

14. Student Exercises

ExerciseChangeQuestion
1Set k = 0.50 W/(m·K)How does lower conductivity change total heat transfer?
2Double wall thicknessHow much does heat transfer decrease?
3Set emissivity to 0.20How does the radiation contribution change?
4Increase houtWhat happens to the outer-surface temperature?
5Set Tsur = 25°CHow does reducing the radiation temperature difference affect Qrad?
6Change the areaWhich quantities scale with area and which temperatures are controlled by resistances?
7Compare low and high emissivityWhen does radiation become a larger share of heat rejection?
8Change spatial resolutionCompare wall-temperature profiles using 10, 20, 50 and 100 points.

A strong student assignment is to submit the input table, governing equations, MATLAB code, three selected plots, an energy-balance check and a short engineering interpretation.

15. Engineering Applications

The same ideas appear in building envelopes, heat exchangers, electronics cooling, furnaces, boilers, thermal insulation and energy systems. Building walls combine conduction through layers with convection and long-wave radiation at surfaces. Heat exchangers involve convection on fluid sides and conduction through the separating wall. Electronics cooling can involve conduction through the package and heat sink followed by convection and radiation.

For students moving toward CFD, this model is a useful stepping stone. Before solving a full 2D temperature field, it helps to understand boundary conditions, thermal resistance, heat flux, sensitivity analysis and energy conservation.

The Thermal Diffusivity Calculator is useful when moving from steady conduction to transient analysis. The Stefan-Boltzmann Radiation Calculator isolates the radiation equation, while the U-value / R-value Calculator extends thermal resistance to multi-layer envelopes. For HVAC air-side work, the Psychrometric Calculator provides moist-air properties.

16. Conclusion

This MATLAB heat transfer simulation connects three fundamental mechanisms with a practical numerical workflow. The script calculates conduction, convection and radiation, solves the coupled steady-state wall problem with fzero, produces seven plots and checks the energy balance.

The real learning value is the workflow: define the physics, keep units consistent, formulate the equations, solve the unknown boundary condition, visualize the result, vary important parameters and validate the solution. Once this pattern is understood, it can be extended to transient conduction, fins, heat exchangers, thermal-resistance networks and 2D numerical heat-transfer solvers.

Frequently Asked Questions About MATLAB Heat Transfer Simulation

What does this MATLAB heat transfer simulation calculate?

The script demonstrates conduction, convection and radiation separately and then combines them in a steady-state wall model where heat reaches the outer surface by conduction and leaves through convection and radiation.

Which equations are used in the MATLAB heat transfer model?

The tutorial uses Fourier law for conduction, Newton's law of cooling for convection, and the Stefan-Boltzmann equation for radiation. The combined model is solved from a steady-state energy balance.

Why is fzero used in the MATLAB heat transfer simulation?

The radiation term contains absolute temperature raised to the fourth power, so the outer-surface energy balance is nonlinear. MATLAB fzero finds the surface temperature that makes heat entering equal heat leaving.

Why must radiation temperature be converted to Kelvin?

The Stefan-Boltzmann equation uses absolute temperature. Celsius values must therefore be converted to Kelvin before evaluating the fourth-power temperature terms.

Can I change the wall thickness and material in the MATLAB code?

Yes. Change L for wall thickness and k for thermal conductivity in the input section, then rerun the script. The wall-thickness plot updates automatically.

Can this model be used for a real engineering design?

It is suitable for learning, preliminary analysis and sensitivity studies. Detailed design may require temperature-dependent properties, contact resistance, view factors, transient effects, multidimensional conduction and validated standards.

Author and Technical Note

About the author: Vikas Sharma is an engineering researcher and technical writer working across CFD, heat transfer, HVAC, building energy and engineering simulation. This tutorial is intended for education, preliminary analysis and numerical-learning exercises. Detailed engineering design should use validated material properties, applicable standards and project-specific boundary conditions.

Authoritative External References

Embedded figures: The seven MATLAB result plots are embedded directly in this HTML as PNG data. If Blogger strips data-image sources when saving the post, upload the seven PNG files to Blogger and replace the corresponding image source with the generated Blogger image URL.

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