SIMVehiclesSubmodules

Aerodynamics submodule

Use aerodynamic parameters to model drag, lift, ride-height dependency, speed dependency, and yaw dependency for a vehicle setup.

Aerodynamics define the drag and lift model used by SIM. Use this submodule when a vehicle setup needs aero coefficients, ride-height maps, or speed and yaw corrections.

When to use it

Use aerodynamics when you need a reusable setup building block that can be selected in a vehicle assembly. Create and maintain it from Design > Aerodynamics, then select it in the vehicle slot Aerodynamics.

How it fits vehicle setup

  1. Create or duplicate the submodule from the Design section.
  2. Open the submodule row to review and edit parameter values.
  3. Save changes with Update Data.
  4. Open Vehicles and select the submodule in Vehicle Assembly.
  5. Use the vehicle detail tabs to inspect the selected submodule inside the vehicle context.

You need module create permission to create a new submodule and module update permission to edit values.

Parameter reference

Units, defaults, and ranges show n/a when no stable user-facing value was verified in the source used for this page. Method rows control which constant, lookup table, or polynomial rows are active in the product table.

General

ParameterDescriptionUnitsDefaultValidation / Range
Frontal AreaThe cross sectional area of the car seen from the front.n/an/a
Cd OffsetA possibility to offset the aerodynamic drag coefficient (for example from different wing settings or other add-on features like blanking etc). This offset will be applied on all of the various options that are available to define the aerodynamic drag coefficient (constant, lookup table or polynomial).n/an/an/a
Clf OffsetA possibility to offset the aerodynamic lift coefficient for the front axle (for example from different wing settings or other add-on features like blanking etc). This offset will be applied on all of the various options that are available to define the aerodynamic lift coefficient (constant, lookup table or polynomial).n/an/an/a
Clr OffsetA possibility to offset the aerodynamic lift coefficient for the rear axle (for example from different wing settings or other add-on features like blanking etc). This offset will be applied on all of the various options that are available to define the aerodynamic lift coefficient (constant, lookup table or polynomial).n/an/an/a

Ride height dependency

ParameterDescriptionUnitsDefaultValidation / Range
MethodThe selector that defines if aerodynamic forces shall be calculated by the simple constant values or by the more detailed aero map lookup tables or by the two dimensional polynomial functions.n/an/aSelects active input method
Cd ConstantThe constant value for aerodynamic drag. Always a positive value.n/an/aVisible when method = Constant
Clf ConstantThe constant value for aerodynamic lift on the front axle. A positive value means that the car will have less load on the front axle with increasing vehicle speed. A car with "downforce" will accordingly have a negative coefficient.n/an/aVisible when method = Constant
Clr ConstantThe constant value for aerodynamic lift on the rear axle. A positive value means that the car will have less load on the rear axle with increasing vehicle speed. A car with "downforce" will accordingly have a negative coefficient.n/an/aVisible when method = Constant
Cd Lookup TableLookup table defining the aerodynamic drag coefficient vs ride height front and ride height rear. Always a positive value.n/an/aVisible when method = LookupTable
Clf Lookup TableLookup table defining the aerodynamic lift coefficient for the front axle vs ride height front and ride height rear. A positive value means that the car will have less load on the front axle with increasing vehicle speed. A car with "downforce" will accordingly have a negative coefficient.n/an/aVisible when method = LookupTable
Clr Lookup TableLookup table defining the aerodynamic lift coefficient for the rear axle vs ride height front and ride height rear. A positive value means that the car will have less load on the rear axle with increasing vehicle speed. A car with "downforce" will accordingly have a negative coefficient.n/an/aVisible when method = LookupTable
Cd PolynomialSecond order two dimensional polynomial coefficients to define the aerodynamic drag coefficient vs ride height front and ride height rear. Cd = c0 + c1 _ rideHeightFront + c2 _ rideHeightRear + c3 _ rideHeightFront _ rideHeightRear + c4 _ rideHeightFront^2 + c5 _ rideHeightRear^2n/an/aVisible when method = Polynomial
Clf PolynomialSecond order two dimensional polynomial coefficients to define the aerodynamic lift coefficient for the front axle vs ride height front and ride height rear. Clf = c0 + c1 _ rideHeightFront + c2 _ rideHeightRear + c3 _ rideHeightFront _ rideHeightRear + c4 _ rideHeightFront^2 + c5 _ rideHeightRear^2n/an/aVisible when method = Polynomial
Clr PolynomialSecond order two dimensional polynomial coefficients to define the aerodynamic lift coefficient for the rear axle vs ride height front and ride height rear. Clr = c0 + c1 _ rideHeightFront + c2 _ rideHeightRear + c3 _ rideHeightFront _ rideHeightRear + c4 _ rideHeightFront^2 + c5 _ rideHeightRear^2n/an/aVisible when method = Polynomial

Speed dependency

ParameterDescriptionUnitsDefaultValidation / Range
Cd PolynomialThird order polynomial coefficients to define the aerodynamic drag variation dependent on vehicle speed. It is added to the aerodynamic drag coefficient defined by any of the methods; constant, lookup table or polynomial. CdDelta = c1 _ vehicleSpeed + c2 _ vehicleSpeed^2 + c3 * vehicleSpeed^3.n/an/ac0 fixed at 0
Clf PolynomialThird order polynomial coefficients to define the aerodynamic lift variation on the front axle dependent on vehicle speed. It is added to the aerodynamic lift coefficient for the front axle defined by any of the methods; constant, lookup table or polynomial. ClfDelta = c1 _ vehicleSpeed + c2 _ vehicleSpeed^2 + c3 * vehicleSpeed^3.n/an/ac0 fixed at 0
Clr PolynomialThird order polynomial coefficients to define the aerodynamic lift variation on the rear axle dependent on vehicle speed. It is added to the aerodynamic lift coefficient for the rear axle defined by any of the methods; constant, lookup table or polynomial. ClrDelta = c1 _ vehicleSpeed + c2 _ vehicleSpeed^2 + c3 * vehicleSpeed^3.n/an/ac0 fixed at 0

Yaw dependency

ParameterDescriptionUnitsDefaultValidation / Range
Cd PolynomialThird order polynomial coefficients to define the aerodynamic drag variation dependent on vehicle yaw angle. It is added to the aerodynamic drag coefficient defined by any of the methods; constant, lookup table or polynomial. CdDelta = c1 _ vehicleYawAngle + c2 _ vehicleYawAngle^2 + c3 * vehicleYawAngle^3.n/an/ac0 fixed at 0
Clf PolynomialThird order polynomial coefficients to define the aerodynamic lift variation on the front axle dependent on vehicle yaw angle. It is added to the aerodynamic lift coefficient for the front axle defined by any of the methods; constant, lookup table or polynomial. ClfDelta = c1 _ vehicleYawAngle + c2 _ vehicleYawAngle^2 + c3 * vehicleYawAngle^3.n/an/ac0 fixed at 0
Clr PolynomialThird order polynomial coefficients to define the aerodynamic lift variation on the rear axle dependent on vehicle yaw angle. It is added to the aerodynamic lift coefficient for the rear axle defined by any of the methods; constant, lookup table or polynomial. ClrDelta = c1 _ vehicleYawAngle + c2 _ vehicleYawAngle^2 + c3 * vehicleYawAngle^3.n/an/ac0 fixed at 0

On this page