aeroPerformanceMap Element

aeroPerformanceMapRCType

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
Sequence Sequence
      Element atmosphericModel

Atmospheric model and temperature offset

      Element machNumber

Mach number

      Element altitude

Altitude

      Element angleOfSideslip

Sideslip angle

      Element angleOfAttack

Angle of attack

      Element analysisTool[0, 1]

Name and version of the tool used to compute the aerodynamic performance

      Element analysisLevel[0, 1]

Modeling level of the methods used to compute the aerodynamic performance. The higher the analysisLevel, the higher the quality of the results. Possible use of analysisLevel: 0- 9 = Statistical models, 10-19 = Analytic models, 20-29 = Lifting line method, 30-39 = Panel method, 40-49 = Panel-BL-coupled method, 50-59 = Full potential method, 60-69 = Full potential-BL coupled method, 70-79 = CFD euler method, 80-89 = CFD euler-bl coupled method, 99-99 = CFD RANS method, >=100 = Experimental data.

      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

Attributes
NameTypeRequiredDescription
Attribute externalDataDirectorySimple Type string
Attribute externalDataNodePathSimple Type string
Attribute externalFileNameSimple Type string
Remarks
AeroPerformanceMapRC type, containing a perfomance map with aerodynamic data. Array order is: angleOfAttack min->max then angleOfSideslip then altitude then machNumber
See Also