element · restriction xsd:double
Trailing edge thickness
Total trailing edge thickness relative to the chord length. A value of 0 gives a closed trailing edge; without this element, the airfoil follows the original NACA definition.
| Constraint | Value |
|---|---|
| minInclusiveThe value must be this or greater. | 0 |
cpacs/vehicles/profiles/fuselageProfiles/fuselageProfile/nacaProfile/trailingEdgeThicknesscpacs/vehicles/profiles/wingAirfoils/wingAirfoil/nacaProfile/trailingEdgeThicknesscpacs/vehicles/profiles/rotorAirfoils/rotorAirfoil/nacaProfile/trailingEdgeThickness| Type | Name |
|---|---|
nacaProfileType | trailingEdgeThickness |