Calculator overview
Inputs and outputs
This summary comes from the calculator's published input and output contract.
Inputs
- CWT Hot Side Film Coefficient Conditional
-
Unit W/(m^2*K) Default 137.3 Range At least 0
About this input
Positive user-entered hot-side heat-transfer coefficient used only with bulk-fluid boundary temperatures. No correlation or lookup is provided; the shipped value is a synthetic arithmetic demonstration.
- Hot-side surface temperature
-
Unit deg C Default 100 Range At least -273.15 (conditional)
About this input
Hot-side surface temperature in surface mode or hot-side bulk-fluid temperature in film mode. The computed lower bound is absolute zero.
- CWT Unit System
-
Default SI metric Allowed SI metric, US customary
About this input
Select a coherent SI or U.S. customary entry path. Grid values and scalar values are not converted automatically when this selector changes.
- Plane-wall layers - thickness (mm), conductivity (W/(m*K))
-
Default 6 rows
About this input
Submit exactly six complete rows. Set Use layer? to Yes for each layer in series and No for unused rows. Every Yes row needs a 1-to-80-character non-whitespace label, positive thickness, and positive conductivity in the selected units. No rows may contain null or empty cells; shipped active thicknesses and conductivities are conspicuously synthetic arithmetic values, while unused rows use a nonblank label, zero thickness, and conductivity 1 as inert transport-safe sentinels. Numeric grid cells are transported as strings under contract 0.17 and are parsed explicitly.
Column Range or allowed values Use layer? No, Yes Layer label Not declared Thickness At least 0 Thermal conductivity At least 0 - Cold-side surface temperature
-
Unit deg C Default 20 Range At least -273.15 (conditional)
About this input
Cold-side surface temperature in surface mode or cold-side bulk-fluid temperature in film mode. It must not exceed the hot-side boundary temperature.
- CWT Boundary Temperature Basis
-
Default Known surface temperatures Allowed Known surface temperatures, Known bulk-fluid temperatures with entered film coefficients
About this input
Use known wall-surface temperatures for solid conduction only, or use bulk-fluid temperatures and add two positive user-entered film coefficients.
- CWT Heat Transfer Area
-
Unit m^2 Default 10 Range At least 0
About this input
Positive area normal to heat flow, common to every active plane layer. Variable-area and radial geometries are outside scope.
- CWT Cold Side Film Coefficient Conditional
-
Unit W/(m^2*K) Default 31.7 Range At least 0
About this input
Positive user-entered cold-side heat-transfer coefficient used only with bulk-fluid boundary temperatures. No correlation or lookup is provided; the shipped value is a synthetic arithmetic demonstration.
Outputs
- CWT Total Areal Resistance
-
Unit m^2*K/W
About this output
Total solid resistance plus two entered 1/h film resistances in bulk-fluid mode; equal to solid resistance in surface-temperature mode.
- CWT Overall Thermal Conductance
-
Unit W/(m^2*K)
About this output
Reciprocal of total areal resistance for this idealized plane-wall stack and selected boundary basis.
- CWT Hot Surface Temperature Conditional
-
Unit deg C
About this output
Hot bulk-fluid temperature minus the temperature drop across the entered hot-side film resistance. Hidden in surface-temperature mode because the surface value is already an input.
- Model Status
-
No unit declared
About this output
Returns actionable NOT VALID text for malformed fixed-grid or boundary inputs and derived overflow, CHECK for equal boundary temperatures, and OK otherwise. It does not certify an assembly or select a material.
- CWT Total Solid Thickness
-
Unit mm
About this output
Sum of entered thicknesses for all Yes rows; unused rows contribute zero.
- CWT Total Solid Areal Resistance
-
Unit m^2*K/W
About this output
Sum of thickness divided by conductivity for every active plane-wall layer, excluding any surface-film resistance.
- CWT Heat Transfer Rate
-
Unit kW
About this output
Heat flux multiplied by the entered common plane-wall area. SI results are displayed in kilowatts; the internal SI result is in watts.
- CWT Cold Surface Temperature Conditional
-
Unit deg C
About this output
Cold bulk-fluid temperature plus the temperature rise across the entered cold-side film resistance. Hidden in surface-temperature mode because the surface value is already an input.
- CWT Boundary Basis Used
-
No unit declared
About this output
States whether heat transfer uses entered solid-surface temperatures alone or bulk-fluid temperatures plus two entered film resistances.
- CWT Active Layer Count
-
Unit layers
About this output
Number of six fixed grid rows marked Yes. Noncontiguous and duplicate-labelled active rows count independently.
- CWT Heat Flux
-
Unit W/m^2
About this output
Nonnegative boundary temperature difference divided by total areal resistance.
- CWT Dominant Resistance Layer
-
No unit declared
About this output
First active grid label whose layer resistance equals the maximum active layer resistance.
- CWT Dominant Layer Resistance Share
-
Unit fraction
About this output
Largest active layer areal resistance divided by total solid areal resistance. The structural range is zero through one.
What it is
The Composite Wall Thermal Resistance and Heat Loss Calculator computes the steady one-dimensional heat flux and heat rate through a flat wall built from up to six layers in series. Each layer carries a thickness and a thermal conductivity entered in a fixed six-row grid, with a Yes or No selector saying whether that row is part of the stack, and the wall carries one common area normal to the heat flow.
It reports the total areal resistance with and without the surface films, the overall conductance, the heat flux, the heat rate, the total active thickness, the active layer count, which layer contributes the most resistance and what share of the total it holds, and plots the temperature profile through the stack.
Boundary temperatures are entered on one of two bases. With known surface temperatures the calculation covers the solid stack alone. With known bulk-fluid temperatures you add a film coefficient on each side, the model puts two 1/h resistances in series with the wall, and it returns the wall-surface temperatures it derived. In surface-temperature mode the film fields are hidden and have no effect on any output.
Entry is in SI metric or US customary. The selector relabels the fields and switches the temperature floor. It converts nothing you have already entered, in the grid or anywhere else.
The model is plane and one-dimensional. Contact resistance, thermal bridging through studs, ties and fasteners, edge effects, and any radial or variable-area geometry are outside its scope. The result describes an idealised uninterrupted section, not an assembly as built.
Methodology
Purpose and model boundary
This model calculates steady, one-dimensional heat flow through a constant-area plane wall containing up to six active layers in series. It can begin from known wall-surface temperatures, or from bulk-fluid temperatures with user-entered hot- and cold-side film coefficients. It does not select materials, estimate film coefficients, or perform transient, moisture, fire, or code analysis.
Inputs and units
The unit-system selector controls the displayed temperature, thickness, area, conductivity, film-coefficient, resistance, flux, and heat-rate units. The wall table contains exactly six rows; active rows require a label, positive thickness, and positive thermal conductivity. Inactive rows remain part of the fixed submitted values but are excluded from the thermal path. Bulk-fluid mode also uses both positive film coefficients. Surface-temperature mode excludes the film resistances.
Governing relationships
For active layer i, the areal conduction resistance is:
R_i = L_i / k_i
The solid resistance and thickness are:
R_solid = Σ R_i
L_total = Σ L_i
When bulk-fluid temperatures are selected, the two film resistances are:
R_hot-film = 1 / h_hot
R_cold-film = 1 / h_cold
The selected total resistance, conductance, heat flux, and heat rate are:
R_total = R_solid in surface-temperature mode
R_total = 1/h_hot + R_solid + 1/h_cold in bulk-fluid mode
U = 1 / R_total
q'' = (T_hot - T_cold) / R_total
Q = A × q''
Interface temperatures are found by subtracting the heat-flux times the cumulative resistance from the hot-side temperature. The chart plots that workbook-calculated interface profile against cumulative active thickness.
Calculation sequence
- Validate the selected unit and boundary modes, temperature order, area, active layer rows, and any active film coefficients.
- Convert values to the workbook's common calculation basis.
- Sum active
L/kterms and, when selected, the two1/hterms. - Calculate
U, heat flux, total heat rate, surface temperatures, and each layer-interface temperature. - Identify the active layer with the largest resistance and its share of the solid resistance.
- Evaluate the workbook status in the precedence shown below.
Outputs and interpretation
Heat flux and total heat-transfer rate are the headline results. Supporting outputs expose total and solid-only areal resistance, overall conductance, active-layer count and total thickness, hot/cold surface temperatures, the selected boundary basis, and the dominant resistance layer. The dominant-layer result is a resistance comparison, not a material recommendation.
Validation and status logic
| Condition, evaluated in order | Returned status |
|---|---|
| A selection, boundary temperature, area, active film coefficient, or six-row layer input is invalid | NOT VALID: correct visible boundary, area, film, or six-row layer inputs |
| A derived numeric result exceeds the workbook's supported calculation range | NOT VALID: derived result exceeds the supported calculation range |
| The hot and cold boundary temperatures are equal | CHECK: equal boundary temperatures produce zero heat transfer |
| None of the preceding conditions applies | OK |
The status formula above was verified against the workbook's named Model_Status calculation. Invalid states publish protected zero-valued numeric outputs rather than Excel error tokens; those zeros must not be interpreted as physical results.
Assumptions and limitations
- Heat transfer is steady and normal to a plane wall with the same area through every layer.
- Each layer is homogeneous, has constant conductivity, has no internal heat generation, and is in perfect contact with adjacent layers.
- Cylindrical, spherical, radial, finned, tapered, multidimensional, and thermal-bridge geometries are outside scope.
- Radiation, moisture transport, contact resistance, gaps, edge loss, phase change, temperature-dependent properties, and transient storage are not modeled.
- The workbook contains no material-property, insulation, film-coefficient, or assembly U-value library. All properties are user-entered.
Restrictions and non-computing states
This calculator requires exactly six complete layer rows. Active rows need nonblank 1-to-80-character labels and positive thickness/conductivity. At least one layer must be active. The hot-side temperature cannot be below the cold-side temperature, area must be positive, and film coefficients must be positive whenever bulk-fluid mode makes them active. Values outside the published limits are rejected before the calculation runs.
Errors and warnings
NOT VALID means the visible state cannot form a supported wall calculation. CHECK preserves a valid zero-driving-force result but asks the reader to confirm that the equal temperatures are intentional. A connection, publishing, or calculation-service error is not a thermal result and must not be read as zero heat loss.
References
The equations, status precedence, visibility rules, and output roles were checked against the delivered workbook, its published input rules, tests, reviewer packet, and formulas bound to the named outputs. The workbook identifies these technical sources:
- DOE-HDBK-1012/2-92, Thermodynamics, Heat Transfer, and Fluid Flow, Volume 2 — Fourier conduction, series thermal resistance, and heat-transfer relationships.
- NASA, Introduction to Numerical Methods in Heat Transfer — Independent confirmation of steady one-dimensional Fourier conduction.
- NIST Guide to the SI, Appendix B — Exact unit conversions used by the SI/US modes.
Frequently asked questions
Why do my film coefficients make no difference?
Will my real wall perform as well as this says?
Which layer should I make thicker?
I switched to US customary and the answer changed. Is that a bug?
Why did it refuse a hot side colder than my cold side?
What are the rules for the layer grid?
Why did every number come back as zero?
Why does the profile chart end in a flat line?
Can I trust the dominant-layer label?
Found a problem, or have an idea?
Tell us if a result looks wrong, a label is unclear, or something is missing. We read every message.
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