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aeroPerformanceMap Element

Aerodynamic coefficients and derivatives

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
All All
      Element altitude

Altitude [m]

      Element angleOfAttack

Angle of attack [deg]

      Element angleOfSideslip

Sideslip angle [deg]

      Element cd[0, 1]

Drag coefficient in aerodynamic coordinates

      Element cl[0, 1]

Lift coefficient in aerodynamic coordinates

      Element cmd[0, 1]

Aerodynamic moment around d-axis of the aerodynamic coordinate system

      Element cml[0, 1]

Aerodynamic moment around l-axis of the aerodynamic coordinate system

      Element cms[0, 1]

Aerodynamic moment around s-axis of the aerodynamic coordinate system

      Element cs[0, 1]

Coefficient of the side force vector in aerodynamic coordinates (perpendicular to lift and drag)

      Element dampingDerivatives[0, 1]

Damping derivatives with respect to the rotational rates

      Element incrementMaps[0, 1]

Increments of the aerodynamic coefficients due to movable device deflections

      Element machNumber

Mach number

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

See Also

Reference

aeroMapType