PORTANCE aérodynamique hydrodynamique coefficients portancePORTANCE aérodynamique hydrodynamique coefficients portance

aerodynamique lift

Voir aussi:

Modeling wings or foils in heliciel Model a mast wing sail in heliciel

Aerodynamics Hydrodynamics web app: aerodynamics-hydrodynamics-database

Lift and CL (lift coefficient)


The aerodynamic or hydrodynamic lift is a force perpendicular to the movement of the fluid. It is created by the suction in a negative pressure zone, formed on top of the profile designed for this purpose. It depends on the displaced mass of fluid.

The lift is calculated according :

Cz or lift coefficient is measured in a wind tunnel and there are databases available for many profiles, which provide performance at different speeds and different incidences.

lthe lift is in general necessary to fly the wing with its load strength. It is linked to the drag which will be compensated by a thrust at least equal to take off

In the case of profiles measured in the wind tunnel, the lift is calculated according to wing surface.

lift formula

In his profile editor, Mecaflux Standard integrates Xfoil to determine profiles lift and drag

The explanation of the phenomenon of aerodynamic or hydrodynamic lift can be partly given, by the variation of the fluid speed , between the lower and upper surfaces.This change in speed causes a change in pressure (see Bernoulli) that generates lift.

fluid path around the profile

In this animations below, of the fluid path around a cylinder and around a profile, you can see the difference in speed generated for :

A profile of zero lift incidence, and a fixed cylinder: equivalent fluid path between the lower and upper surfaces => no pressure difference=>no lift

Profile incidence zero liftFixed cylinder lift

Below is a profile with incidence and a rotating cylinder: longer fluid path on the underside than on the upper surface=> difference in speed=>pressure difference=> Lift

lift incidence profilerotating cylinder

The rotation of the cylinder causes an overspeed on top of the cylinder, the speed increase creates a vacuum within the fluid, which causes the lift.

This approach is very simplified to deepen the theory of lift, see : Lifting line theory on Heliciel.com


The Mecaflux standard software offers 11 different profiles to 8 angles of incidence and 3 ranges of Reynolds numbers and extrapolations

lift and drag interface of mecaflux standard software

If that is not enough you have a profile editor allows you to build your profile files and integrate them into the calculation of lift

editor Aerodynamic and hydrodynamic Lift

See also: create the wing 3D file



charge hydrostatique derive aerodynamique hydrodynamique construire aile foil construire eolienne dimensionner conduits fumée carene dirigeable construire helice propulsion derive aerodynamique hydrodynamique frottement sur une surface de coque trainée resistance au vent trainée resistance au vent construire eolienne trainée resistance au vent conception helice bateaux derive aerodynamique hydrodynamique carene dirigeable frottement sur une surface de coque construire aile foil construire aile foil conception hydrolienne calcul voile frottement sur une surface de coque trainée resistance au vent calcul voile construire aile foil construire eolienne construire helice propulsion aeraulique aspiration air systemes ventilation aeration pertes charges vannes debit et pression conduits pompes et ventilateurs vidange reservoir construire aile foil Logiciels de la suite Mecaflux Forces sur des objets géometriques dans un courant de fluide ramification et boucles réseaux dimensionner conduits fumée calcul systemes réseaux fluides gaz liquides helice a vitesse nulle sustentation resistance aerodynamique vehicules calcul debit rivierre helice de captage turbine Kaplan hydroelectrique charge hydrostatique carene dirigeable construire helice propulsion derive aerodynamique hydrodynamique