aeroPerformanceMap Element

aeroPerformanceMapType

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
Sequence Sequence
      Element machNumber

Mach number

      Element reynoldsNumber

Reynolds Number

      Element angleOfYaw

Yaw angle

      Element angleOfAttack

Angle of attack

      Element cfx[0, 1]

stringArrayBaseType

      Element cfy[0, 1]

stringArrayBaseType

      Element cfz[0, 1]

stringArrayBaseType

      Element cmx[0, 1]

stringArrayBaseType

      Element cmy[0, 1]

stringArrayBaseType

      Element cmz[0, 1]

stringArrayBaseType

      Element dampingDerivatives[0, 1]

Damping derivatives for positive and negative rotation rates

      Element controlSurfaces[0, 1]

controlSurfacePerformanceMaps

      Element landingGears[0, 1]

aeroLandingGearsType

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
Remarks
AeroPerformanceMap type, containing a perfomance map with aerodynamic data. Array order is: angleOfAttack min->max then angleOfYaw then reynoldsNumber then machNumber.All coefficients in the aeroperformanceMap relate to the CPACS coordinate system. See documentation of the CPACS-Element for further information.
See Also