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wingCellType Complex Type

Cell of the wing

Namespace: Empty

Schema: Empty

Base Type
Usages
Children
NameOccurrencesDescription
All All
      Element positioningInnerBorder

Spanwise position of the inner border of the cell

      Element positioningLeadingEdge

Chordwise position of the leading edge border of the cell

      Element positioningOuterBorder

Spanwise position of the outer border of the cell

      Element positioningTrailingEdge

Chordwise position of the trailing edge border of the cell

      Element skin

Skin

      Element stringer[0, 1]

Stringers of the cell

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string

Directory of the external data file

Attribute externalDataNodePathSimple Type string

Path of the node inside the external data file

Attribute externalFileNameSimple Type string

Name of the external data file

Attribute uIDSimple Type IDYes

UID

Remarks

A cell defines a special region of the wing. Within this region skin and stringer properties can be defined that differer from the properties of the rest of the wing. In general a cell is defined by defining four borders – the cell leading and trailing edge and the inner border and the outer border. Those borders can either be defined by using eta/xsi coordinates or by referencing to spars and ribs. Mixed definitions (e.g. forward border is defined due to a spar, side borders due to eta coordinates) is allowed. In general a cell is quadrilateral. But if e.g. the spar, which is used for the definition of the trailing edge, has a kink, the cell can have more than four corners.

The cell leading and trailing edge (= forward and rear border) can either be defined by referencing to a spar (->sparUID) or by the defining the xsi (=relative chord) coordinates of the border (xsi1 = inner end; xsi2 = outer end).

The cell inner and outer border can either be defined by referencing to a rib (->ribDefinitionUID and ribNumber) or by the defining the eta (=relative spanwise) coordinates of the border (eta1 = forward end; eta2 = rear end).

Some examples for wing cells can be found in the picture below:

cells