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Stiffness does not rise gently as it gets colder — it rises exponentially, and the cloth is fine right up until it is not.
Rigidity at Service Temperature
—mN·cm
Projected on the exponential stiffening law
Cold Behaviour
Stiffening Factor
—×
Margin to Cracking Threshold
—mN·cm
Threshold Consumed
—%
Cold Crack Temperature
—°C
Rigidity per mm Thickness
—mN·cm/mm
Extrapolating an exponential fit far below the measured range is unreliable — near the glass transition the curve steepens sharply and the real crack temperature arrives earlier than this predicts. Fit the coefficient from measurements bracketing the service temperature, and confirm by cold bend test to the governing standard.
Using this calculator
About the Coated Fabric Low-Temperature Flexural Rigidity Predictor
The formula
This is the expression the tool evaluates. Every term is named underneath, with the unit it must be supplied in.
Rigidity at Service TemperaturelowTempRigidity = f( referenceRigidity, referenceTemp, betaPerDegree, testTemp, crackThreshold, thickness )
Each input feeds the expression evaluated in the browser; the symbol table below names every term and its unit.
Symbols used above
Symbol
Stands for
Unit
referenceRigidity
Rigidity at Reference
mN·cm
referenceTemp
Reference Temperature
°C
betaPerDegree
Stiffening Coefficient
per °C
testTemp
Service Temperature
°C
crackThreshold
Cracking Rigidity Threshold
mN·cm
thickness
Coated Fabric Thickness
mm
lowTempRigidity
Rigidity at Service Temperature
mN·cm
rigidityIncrease
Stiffening Factor
×
margin
Margin to Cracking Threshold
mN·cm
utilisation
Threshold Consumed
%
criticalTemperature
Cold Crack Temperature
°C
specificRigidity
Rigidity per mm Thickness
mN·cm/mm
How the result is derived
Step by step, from the values you type to the figure on screen.
The 6 inputs are read from the form on every keystroke: Rigidity at Reference, Reference Temperature, Stiffening Coefficient, Service Temperature, Cracking Rigidity Threshold and Coated Fabric Thickness.
Each value is checked against the accepted range in the input table below. A value outside its range stops the calculation rather than producing a misleading figure — the results blank out and a message appears.
The validated values are substituted into the expression above, which resolves Rigidity at Service Temperature together with every supporting figure in one pass — no value is carried over from a previous entry.
The supporting outputs — Stiffening Factor, Margin to Cracking Threshold, Threshold Consumed, Cold Crack Temperature and Rigidity per mm Thickness — come from the same pass, so they always describe the same case as the headline figure.
Results are rounded for display only. The full-precision value is used throughout the chain, so reading a rounded intermediate figure back into the tool by hand can shift the last digit.
What each input means
Where to read each value on the floor, the unit it must be in, and the range the tool accepts.
Input
Unit
Accepted range
Default
What it means
Rigidity at Reference
mN·cm
0.1 to 500 mN·cm
15
Reference Temperature
°C
0 to 40 °C
23
Stiffening Coefficient
per °C
0.005 to 0.2 per °C
0.045
Fitted from rigidity measured at two temperatures.
Service Temperature
°C
-80 to 30 °C
-30
Cracking Rigidity Threshold
mN·cm
10 to 2000 mN·cm
180
Coated Fabric Thickness
mm
0.05 to 10 mm
0.8
What the tool returns
The headline figure and every supporting value it is built from.
Output
Unit
What it tells you
Rigidity at Service Temperature (headline result)
mN·cm
Projected on the exponential stiffening law
Stiffening Factor
×
Margin to Cracking Threshold
mN·cm
Threshold Consumed
%
Cold Crack Temperature
°C
Rigidity per mm Thickness
mN·cm/mm
Worked example
Given
Rigidity at Reference
15 mN·cm
Reference Temperature
23 °C
Stiffening Coefficient
0.045 per °C
Service Temperature
-30 °C
Cracking Rigidity Threshold
180 mN·cm
Coated Fabric Thickness
0.8 mm
The tool loads with this case already solved — the Rigidity at Service Temperature shown above is its answer. Change one value and the difference from this baseline is the sensitivity of the result to that variable.
How to use it
Work through the input groups in order — Reference Measurement and Service Condition. The defaults are a realistic case, so you can change one value at a time and watch what moves.
There is no calculate button. Every figure recalculates as you type or drag, which is what makes this usable for a what-if sweep rather than a single answer.
Read Rigidity at Service Temperature in the dark results panel — that is the headline figure, expressed in mN·cm.
Check the supporting rows underneath (Stiffening Factor, Margin to Cracking Threshold, Threshold Consumed, Cold Crack Temperature and Rigidity per mm Thickness) before acting on the headline — they are where an implausible input usually shows itself first.
Reset to defaults returns every field to the reference case, which is the quickest way to check whether a surprising result came from the tool or from an input you had changed earlier.
Where this is used
Process planning — establishing Rigidity at Service Temperature before a trial is booked, so machine time and material in Leather, Coated Fabrics & Tarpaulins are committed against a calculated figure rather than an estimate.
Costing and quotation — Rigidity at Service Temperature is an input to the cost sheet, and quoting from a worked number rather than a remembered one is what keeps a margin intact.
Troubleshooting — when the floor result drifts from plan, entering the measured values (starting with Rigidity at Reference) shows how much of the gap in Rigidity at Service Temperature each variable explains.
Teaching and study — the accepted ranges bracket normal Leather, Coated Fabrics & Tarpaulins practice, so moving one variable at a time shows the shape of the relationship rather than a single answer.
Assumptions and limits
Extrapolating an exponential fit far below the measured range is unreliable — near the glass transition the curve steepens sharply and the real crack temperature arrives earlier than this predicts. Fit the coefficient from measurements bracketing the service temperature, and confirm by cold bend test to the governing standard.
Every input is bounded to the range normal practice occupies (Rigidity at Reference 0.1 to 500 mN·cm, Reference Temperature 0 to 40 °C and Stiffening Coefficient 0.005 to 0.2 per °C, and so on for the rest). Those bounds are guard rails against typing errors, not a claim that the formula fails one unit outside them.
The calculation is deterministic: the same inputs always give the same result. It carries no allowance for machine condition, operator skill, ambient conditions or lot-to-lot material variation unless an input above explicitly represents one.
Nothing is sent anywhere. The maths runs in your browser, so the numbers you type never leave the page.
Questions people ask
What do I need to know before using the Coated Fabric Low-Temperature Flexural Rigidity Predictor?
Have these to hand: Rigidity at Reference, Reference Temperature, Stiffening Coefficient, Service Temperature, Cracking Rigidity Threshold and Coated Fabric Thickness. With those entered, the tool returns Rigidity at Service Temperature immediately.
What exactly is Rigidity at Service Temperature?
Projected on the exponential stiffening law. It is reported in mN·cm. It is derived from Rigidity at Reference, Reference Temperature, Stiffening Coefficient, Service Temperature, Cracking Rigidity Threshold and Coated Fabric Thickness, and is the figure the rest of the Leather, Coated Fabrics & Tarpaulins calculation is built around.
Which units does this calculator expect?
Enter Rigidity at Reference in mN·cm, Reference Temperature in °C, Stiffening Coefficient in per °C, Service Temperature in °C, Cracking Rigidity Threshold in mN·cm and Coated Fabric Thickness in mm. Mixing unit systems is the most common cause of a result that looks an order of magnitude wrong — convert before typing, not after reading.
What are the other figures under the main result?
They are the intermediate quantities the calculation passes through: Stiffening Factor, Margin to Cracking Threshold, Threshold Consumed, Cold Crack Temperature and Rigidity per mm Thickness. They are shown because a headline number nobody can trace is a number nobody trusts — checking them against your own expectation is the fastest way to confirm the inputs were read as you intended.
Can I rely on this for a production decision?
Extrapolating an exponential fit far below the measured range is unreliable — near the glass transition the curve steepens sharply and the real crack temperature arrives earlier than this predicts. Fit the coefficient from measurements bracketing the service temperature, and confirm by cold bend test to the governing standard. Treat the output as an engineering estimate that narrows the trial window, not as a substitute for the trial.