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Spunbond Spinline Draw-Down & Aerodynamic Drag

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See what it looks like

Drag goes as the square of slip, and slip collapses as the filament speeds up. Attenuation limits itself.

Spinneret & Polymer What is extruded
g/hole/min
dpf
mm
g/cm3
Aspirator Air Which does the drawing
m/min
kg/m3
Cd

Axial flow along a fine filament, not bluff-body drag

m

Draw-Down Ratio

— x

Final velocity over extrusion velocity

Velocity, Diameter & Force

Mass per Metre of Filament
— mg/m
Extrusion Velocity
— m/min
Final Filament Velocity
— m/min
Final Filament Diameter
— um
Slip Velocity
— m/s
Slip as Share of Air Speed
— %
Drag per Metre of Filament
— mN/m
Total Drag Force
— mN
Spinline Stress
— MPa
Throughput per Hole
— kg/h

This is a lumped balance at the end of the spinline, not a solution of the coupled momentum, energy and crystallisation equations that actually govern it: the real filament accelerates, cools and crystallises together, the drag coefficient varies along its length with local Reynolds number, and stress-induced crystallisation eventually arrests the draw entirely. Treat the stress figure as an order-of-magnitude check on whether the aspirator can plausibly deliver the draw-down being asked of it, not as a design value. Final velocity is derived from mass conservation and the target denier, which means it is the velocity the process MUST reach to make that denier rather than a prediction that it will; where the computed drag looks small against the stress required, the honest reading is that the denier is not achievable at that air setting. The skin friction coefficient is the least certain input and depends strongly on filament Reynolds number and on whether neighbouring filaments are shielding each other, which they are in any real spinneret. Nothing here treats filament-to-filament interaction, drag-induced whipping instability, or the quench that sets the crystalline structure and therefore the tenacity of the finished web.

Using this calculator

About the Spunbond Spinline Draw-Down & Aerodynamic Drag

The formula

This is the expression the tool evaluates. Every term is named underneath, with the unit it must be supplied in.

Velocity from mass conservation
massPerMetre = denier / 9000 v = throughput / massPerMetre

Denier is grams per nine thousand metres, so the final velocity a target denier demands falls straight out of the throughput.

Drag on a filament in axial flow
F/L = 0.5 x Cd x rhoAir x (vAir - vFilament)^2 x pi x d

Squared in the slip. At 3,500 m/min of air against a 2,250 m/min filament, only 36 percent of the air speed is doing any work.

What the spinline carries
stress = F / A drawDown = vFinal / vExtrusion

A draw-down of several hundred is normal for spunbond and is achieved across less than a metre of free filament.

Symbols used above
SymbolStands forUnit
throughputPerHoleThroughput per Holeg/hole/min
targetDenierTarget Filament Denierdpf
holeDiameterCapillary Diametermm
polymerDensityPolymer Densityg/cm3
airVelocityAir Velocitym/min
airDensityAir Densitykg/m3
dragCoefficientSkin Friction CoefficientCd
dragLengthEffective Drag Lengthm
drawDownRatioDraw-Down Ratiox
massPerMetreMass per Metre of Filamentmg/m
extrusionVelocityExtrusion Velocitym/min
finalVelocityFinal Filament Velocitym/min
finalDiameterFinal Filament Diameterum
slipVelocitySlip Velocitym/s
slipShareOfAirSlip as Share of Air Speed%
dragPerMetreDrag per Metre of FilamentmN/m
totalDragForceTotal Drag ForcemN
spinlineStressSpinline StressMPa
throughputPerHoleHourThroughput per Holekg/h

How the result is derived

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

  1. The 8 inputs are read from the form on every keystroke: Throughput per Hole, Target Filament Denier, Capillary Diameter, Polymer Density, Air Velocity, Air Density, Skin Friction Coefficient and Effective Drag Length.
  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 Draw-Down Ratio together with every supporting figure in one pass — no value is carried over from a previous entry.
  4. The supporting outputs — Mass per Metre of Filament, Extrusion Velocity, Final Filament Velocity, Final Filament Diameter, Slip Velocity, Slip as Share of Air Speed, Drag per Metre of Filament, Total Drag Force, Spinline Stress and Throughput per Hole — 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
Throughput per Holeg/hole/min0.02 to 5 g/hole/min0.55
Target Filament Denierdpf0.3 to 20 dpf2.2
Capillary Diametermm0.1 to 2 mm0.35
Polymer Densityg/cm30.7 to 1.6 g/cm30.91
Air Velocitym/min500 to 12000 m/min3500
Air Densitykg/m30.6 to 1.5 kg/m31.2
Skin Friction CoefficientCd0.002 to 0.2 Cd0.02Axial flow along a fine filament, not bluff-body drag
Effective Drag Lengthm0.05 to 3 m0.6

What the tool returns

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

OutputUnitWhat it tells you
Draw-Down Ratio (headline result)xFinal velocity over extrusion velocity
Mass per Metre of Filamentmg/m
Extrusion Velocitym/min
Final Filament Velocitym/min
Final Filament Diameterum
Slip Velocitym/s
Slip as Share of Air Speed%
Drag per Metre of FilamentmN/m
Total Drag ForcemN
Spinline StressMPa
Throughput per Holekg/h

Worked example

Given

Throughput per Hole
0.55 g/hole/min
Target Filament Denier
2.2 dpf
Capillary Diameter
0.35 mm
Polymer Density
0.91 g/cm3
Air Velocity
3500 m/min
Air Density
1.2 kg/m3
Skin Friction Coefficient
0.02 Cd
Effective Drag Length
0.6 m

The tool loads with this case already solved — the Draw-Down Ratio 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 — Spinneret & Polymer and Aspirator Air. 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 Draw-Down Ratio in the dark results panel — that is the headline figure, expressed in x.
  4. Check the supporting rows underneath (Mass per Metre of Filament, Extrusion Velocity, Final Filament Velocity, Final Filament Diameter, Slip Velocity, Slip as Share of Air Speed, Drag per Metre of Filament, Total Drag Force, Spinline Stress and Throughput per Hole) 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 Draw-Down Ratio before a trial is booked, so machine time and material in Nonwovens, Filtration, Hygiene & Technical Webs are committed against a calculated figure rather than an estimate.
  • Costing and quotation — Draw-Down Ratio 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 Throughput per Hole) shows how much of the gap in Draw-Down Ratio each variable explains.
  • Teaching and study — the accepted ranges bracket normal Nonwovens, Filtration, Hygiene & Technical Webs practice, so moving one variable at a time shows the shape of the relationship rather than a single answer.

Assumptions and limits

  • This is a lumped balance at the end of the spinline, not a solution of the coupled momentum, energy and crystallisation equations that actually govern it: the real filament accelerates, cools and crystallises together, the drag coefficient varies along its length with local Reynolds number, and stress-induced crystallisation eventually arrests the draw entirely. Treat the stress figure as an order-of-magnitude check on whether the aspirator can plausibly deliver the draw-down being asked of it, not as a design value. Final velocity is derived from mass conservation and the target denier, which means it is the velocity the process MUST reach to make that denier rather than a prediction that it will; where the computed drag looks small against the stress required, the honest reading is that the denier is not achievable at that air setting. The skin friction coefficient is the least certain input and depends strongly on filament Reynolds number and on whether neighbouring filaments are shielding each other, which they are in any real spinneret. Nothing here treats filament-to-filament interaction, drag-induced whipping instability, or the quench that sets the crystalline structure and therefore the tenacity of the finished web.
  • Every input is bounded to the range normal practice occupies (Throughput per Hole 0.02 to 5 g/hole/min, Target Filament Denier 0.3 to 20 dpf and Capillary Diameter 0.1 to 2 mm, 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 Spunbond Spinline Draw-Down & Aerodynamic Drag?

Have these to hand: Throughput per Hole, Target Filament Denier, Capillary Diameter, Polymer Density, Air Velocity, Air Density, Skin Friction Coefficient and Effective Drag Length. With those entered, the tool returns Draw-Down Ratio immediately.

What exactly is Draw-Down Ratio?

Final velocity over extrusion velocity. It is reported in x. It is derived from Throughput per Hole, Target Filament Denier, Capillary Diameter, Polymer Density, Air Velocity, Air Density, Skin Friction Coefficient and Effective Drag Length, and is the figure the rest of the Nonwovens, Filtration, Hygiene & Technical Webs calculation is built around.

Which units does this calculator expect?

Enter Throughput per Hole in g/hole/min, Target Filament Denier in dpf, Capillary Diameter in mm, Polymer Density in g/cm3, Air Velocity in m/min, Air Density in kg/m3, Skin Friction Coefficient in Cd and Effective Drag Length in m. 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: Mass per Metre of Filament, Extrusion Velocity, Final Filament Velocity, Final Filament Diameter, Slip Velocity, Slip as Share of Air Speed, Drag per Metre of Filament, Total Drag Force, Spinline Stress and Throughput per Hole. 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?

This is a lumped balance at the end of the spinline, not a solution of the coupled momentum, energy and crystallisation equations that actually govern it: the real filament accelerates, cools and crystallises together, the drag coefficient varies along its length with local Reynolds number, and stress-induced crystallisation eventually arrests the draw entirely. Treat the stress figure as an order-of-magnitude check on whether the aspirator can plausibly deliver the draw-down being asked of it, not as a design value. Final velocity is derived from mass conservation and the target denier, which means it is the velocity the process MUST reach to make that denier rather than a prediction that it will; where the computed drag looks small against the stress required, the honest reading is that the denier is not achievable at that air setting. The skin friction coefficient is the least certain input and depends strongly on filament Reynolds number and on whether neighbouring filaments are shielding each other, which they are in any real spinneret. Nothing here treats filament-to-filament interaction, drag-induced whipping instability, or the quench that sets the crystalline structure and therefore the tenacity of the finished web. Treat the output as an engineering estimate that narrows the trial window, not as a substitute for the trial.

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