Click or drag to resize
aeroPerformanceMap Element

aeroPerformanceMapRCType

Namespace: Empty

Schema: Empty

Type
Parents
Children
NameOccurrencesDescription
All All
      Element altitude

Altitude

      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 analysisTool[0, 1]

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

      Element angleOfAttack

Angle of attack

      Element angleOfSideslip

Sideslip angle

      Element atmosphericModel

Atmospheric model and temperature offset

      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 machNumber

Mach number

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