Drone flying at night over the Alpine foothills, red and blue vortex trails behind the rotors
PropLab TPLUS ENGINEERING GMBH
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[ DESIGN · CAD · SIMULATION ]

Mission-based propeller design.From 1D design to simulation.

PropLab designs drone propellers based on your mission profile and, if required, assesses them with CFD and FEM analyses – a complete assessment before the first part is manufactured.

Start a design Have your own propeller analysed
VIEW 01 — WAKEBLADE TIP VORTICES, ARTISTICALLY EXAGGERATED

The design process does not deliver a single solution but the Pareto front of all suitable options, calculated for your flight phases, take-off mass and number of rotors.

Z-01Mission power
Z-02Hover power
Z-03Cruise power
Z-04Blade mass
Z-05Noise in dB(A)
§ 01 PROCESS

From mission profile to validated part.

Development in three steps – each building on the previous one and each available separately.
If you already have a geometry, you can go straight to the analysis.

[01]

1D design

Design with the blade element momentum theory (BEMT) for a catalogue of verified airfoils, followed by multi-objective optimisation with a genetic algorithm. Suitable results can be selected interactively from the Pareto front, depending on your priorities.

[02]

CAD model

Complete 3D CAD model as STEP and STL including hub, shaft bore and bolt circle. Sweep and a rounded blade tip are optional and can be shaped interactively – all in the browser.

[03]

CFD and FEM analysis

Flow and structural assessment by our simulation engineers, steady or unsteady – for your selected flight states from hover to forward flight.

§ 02 RESULTS

Simulation results directly in the browser.

The results of your CFD and FEM simulations are presented in our viewer in the browser. There you can explore the various result quantities and fields interactively. All visualisations and animations are already set up, so you can concentrate entirely on the results. No additional software is required.

Each key figure of the simulation is set against the 1D prediction. This shows not only the result itself but also how well the fast design calculation predicted the operating point.

ALL RESULTS: 1D · CFD · FEM
Surface pressure
VIEW — SURFACE PRESSURECFD RESULT: UNSTEADY CALCULATION
§ 03 OWN GEOMETRY

Analyse existing propellers.

If you already have a propeller geometry, simply upload it and have it analysed at the operating points you need. Our team checks every external geometry before the calculation starts.

STEP · IGES · STL · OTHER FORMATS ON REQUEST

Upload geometry →
§ 04 VALIDATION

Limits of validity are clearly stated.

The 1D design is validated against public wind tunnel measurements (UIUC Propeller Data Site). For every method, from the airfoil polar to the noise estimate, the report states the limits of validity. Approximations such as the cruise estimate are marked as such.

§ 05 PRICING

Services

Net prices plus 19% VAT, gross prices below · projects on request

[01] 1D design € 0 FREE WITH AN ACCOUNT

Multi-objective optimisation based on your mission, including Pareto front and design report as PDF.

[02] CAD model € 249€ 296.31 INCL. VAT INCLUDED WITH CFD/FEM

STEP and STL with an engineered hub, optionally with sweep and a rounded tip.

[03] CFD analysis from € 1,490€ 1,773.10 INCL. VAT STEADY · UNSTEADY ON REQUEST

Simulation and evaluation by our engineers, including results in the viewer and a technical report.

[04] FEM analysis € 1,290€ 1,535.10 INCL. VAT STRENGTH · MODAL ANALYSIS

Strength at overspeed, natural frequencies and Campbell diagram.

All prices and scenarios
A PRODUCT OF TPLUS ENGINEERING GMBH

Automated calculation, checked by experienced simulation engineers.

Start a design Request a consultation
Drone flying at night over the Alpine foothills, red and blue vortex trails behind the rotors
PropLab
VIEW 01 — WAKE
[ DESIGN · CAD · SIMULATION ]

Mission-based propeller design.From 1D design to simulation.

PropLab designs drone propellers based on your mission profile and, if required, assesses them with CFD and FEM analyses – a complete assessment before the first part is manufactured.

Start a design Have your own propeller analysed

The design process does not deliver a single solution but the Pareto front of all suitable options, calculated for your flight phases, take-off mass and number of rotors.

Z-01Mission power
Z-02Hover power
Z-03Cruise power
Z-04Blade mass
Z-05Noise in dB(A)
§ 01 PROCESS

From mission profile to validated part.

Three service levels – each building on the previous one, each available separately.
BYOG – Bring Your Own Geometry: if you already have a geometry, you can go straight to the analysis.

[01]

1D design

Design with the blade element momentum theory (BEMT) and a catalogue of 23 verified airfoils, followed by multi-objective optimisation. The result is the Pareto front together with an automatically generated design report.

[02]

CAD model

Complete CAD model as STEP and STL including hub, shaft bore and bolt circle. Sweep and a rounded blade tip are optional.

[03]

CFD and FEM analysis

Flow and structural assessment by our simulation engineers, steady or unsteady – for your selected flight states from hover to forward flight.

§ 02 RESULTS

Simulation results directly in the browser.

Surface pressure
VIEW — SURFACE PRESSURE · CFD RESULT: UNSTEADY CALCULATION

The results of your CFD and FEM simulations are presented in our viewer in the browser. There you can explore the various result quantities and fields interactively. No additional software is required.

Each key figure of the simulation is set against the 1D prediction. This shows not only the result itself but also how well the fast design calculation predicted the operating point.

ALL RESULTS: 1D · CFD · FEM
§ 03 OWN GEOMETRY

Analyse existing propellers.

An existing propeller geometry can be uploaded and analysed at the required operating points. Our team checks every external geometry before the calculation starts.

STEP · IGES · STL
Other formats on request

Upload geometry
§ 04 VALIDATION

Limits of validity are stated openly.

The 1D calculation chain is validated against public wind tunnel measurements (UIUC Propeller Data Site). For every method, from the airfoil polar to the noise estimate, the report states the limits of validity. Approximations such as the cruise estimate are marked as such.

Motor data can also be included, so that current and voltage limits enter the optimisation as constraints.

§ 05 PRICING

Services

Net prices plus 19% VAT, gross prices below · projects on request

[01]1D design€ 0
FREE WITH AN ACCOUNT

Multi-objective optimisation based on your mission, including Pareto front and design report as PDF.

[02]CAD model€ 249€ 296.31 INCL. VAT
INCLUDED WITH CFD/FEM

STEP and STL with an engineered hub, optionally with sweep and a rounded tip.

[03]CFD analysisfrom € 1,490€ 1,773.10 INCL. VAT
STEADY · UNSTEADY ON REQUEST

Simulation and evaluation by our engineers, including result viewer and technical report.

[04]FEM analysis€ 1,290€ 1,535.10 INCL. VAT
STRENGTH · MODAL ANALYSIS

Strength at overspeed, natural frequencies and Campbell diagram.

All prices and scenarios
A PRODUCT OF TPLUS ENGINEERING GMBH

Automated calculation, checked by experienced simulation engineers.

Start a design Request a consultation