complexType · extension complexBaseType · all
Aerodynamic contributions of a chordwise part within a within a wing segment strip
Describes the contributions of a specific par within a wing segment to the total aerodynamic coefficients of a wing segment strip
A chordwise part describes the contributions of a specific chordwise part within a wing <strip> to the total aerodynamic coefficients of this <strip>. It extends spatially between the two <eta> positions of the parent <strip> (see <strip> documentation) and four <xsi> positions in the segment coordinate system. As with the parent stips, only the trailing border (..ToSegmentXsi) of a chordwise part is defined, while the leading border always equals the trailing border of the preceding chordwise part (or 0 for the first part). To account for oblique trailing borders (e.g., to match the aileron on a tapered wing) two different ..ToSegmentXsi positions can be defined, one at the inner border (<innerBorderToSegmentXsi>) and one at the outer border (<outerBorderToSegmentXsi>) of the parent strip. The <innerBorderToSegmentXsi> and <outerBorderToSegmentXsi> of the last chordwise part must be equal to 1.
| Name | Type | Constraints | Use | Default | Description |
|---|---|---|---|---|---|
@externalDataDirectory | xsd:string | optional | Directory of the external file the element was read from, as URI | ||
@externalDataNodePath | xsd:string | optional | Path of the parent element in the merged dataset, at which the element was inserted from an external file | ||
@externalFileName | xsd:string | optional | Name of the external file the element was read from |
| Name | Type | Constraints | OccurrenceHow often the element may appear at this place. The schema writes it as minOccurs and maxOccurs on the declaration. | Default | Description |
|---|---|---|---|---|---|
| allThe children below may appear in any order. Each may appear at most once. | |||||
innerBorderToSegmentXsi | doubleBaseType | [1..1] required | Chordwise coordinate xsi in the segment coordinate system to define the end position of the chordwisePart at the inner eta border | ||
outerBorderToSegmentXsi | doubleBaseType | [1..1] required | Chordwise coordinate xsi in the segment coordinate system to define the end position of the chordwisePart at the outer eta border | ||
coefficients | aeroCaseCoefficientsType | [1..1] required | Aerodynamic coefficients of the chordwise part | ||
reference | coefficientReferenceType | [1..1] required | Reference values the coefficients are related to | ||
cpacs/vehicles/aircraft/model/analyses/loadAnalysis/loadCases/aeroCases/aeroCase/aeroData/vehicle/coefficientsBreakdown/wings/wing/segments/segment/strips/strip/chordwiseParts/partcpacs/vehicles/rotorcraft/model/analyses/loadAnalysis/loadCases/aeroCases/aeroCase/aeroData/vehicle/coefficientsBreakdown/wings/wing/segments/segment/strips/strip/chordwiseParts/part| Type | Name |
|---|---|
chordwisePartsType | part |