Home » Calculators » Finishing & Environment » Leather, Coated Fabrics & Tarpaulins » Coated Fabric Low-Temperature Flexural Rigidity Predictor
Jump to a calculator 618 tools

Coated Fabrics

Coated Fabric Low-Temperature Flexural Rigidity Predictor

Put this calculator on your own site

Paste this where you want the calculator to appear. It works on any site — WordPress, Squarespace, Webflow, Ghost or plain HTML — and needs no JavaScript of yours. It carries a link back here, which is the only thing we ask for it.

See what it looks like

Stiffness does not rise gently as it gets colder — it rises exponentially, and the cloth is fine right up until it is not.

Reference Measurement At room temperature
mN·cm
°C
per °C

Fitted from rigidity measured at two temperatures.

Service Condition Cold
°C
mN·cm
mm

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 Temperature
lowTempRigidity = 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
SymbolStands forUnit
referenceRigidityRigidity at ReferencemN·cm
referenceTempReference Temperature°C
betaPerDegreeStiffening Coefficientper °C
testTempService Temperature°C
crackThresholdCracking Rigidity ThresholdmN·cm
thicknessCoated Fabric Thicknessmm
lowTempRigidityRigidity at Service TemperaturemN·cm
rigidityIncreaseStiffening Factor×
marginMargin to Cracking ThresholdmN·cm
utilisationThreshold Consumed%
criticalTemperatureCold Crack Temperature°C
specificRigidityRigidity per mm ThicknessmN·cm/mm

How the result is derived

Step by step, from the values you type to the figure on screen.

  1. 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.
  2. 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.
  3. 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.
  4. 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.
  5. 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.

InputUnitAccepted rangeDefaultWhat it means
Rigidity at ReferencemN·cm0.1 to 500 mN·cm15
Reference Temperature°C0 to 40 °C23
Stiffening Coefficientper °C0.005 to 0.2 per °C0.045Fitted from rigidity measured at two temperatures.
Service Temperature°C-80 to 30 °C-30
Cracking Rigidity ThresholdmN·cm10 to 2000 mN·cm180
Coated Fabric Thicknessmm0.05 to 10 mm0.8

What the tool returns

The headline figure and every supporting value it is built from.

OutputUnitWhat it tells you
Rigidity at Service Temperature (headline result)mN·cmProjected on the exponential stiffening law
Stiffening Factor×
Margin to Cracking ThresholdmN·cm
Threshold Consumed%
Cold Crack Temperature°C
Rigidity per mm ThicknessmN·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

  1. 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.
  2. 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.
  3. Read Rigidity at Service Temperature in the dark results panel — that is the headline figure, expressed in mN·cm.
  4. 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.
  5. 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.

Scroll to Top