aeroPerformanceMap Element |
aeroPerformanceMapType
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
Sequence | ||
machNumber | Mach number | |
reynoldsNumber | Reynolds Number | |
angleOfYaw | Yaw angle | |
angleOfAttack | Angle of attack | |
analysisTool | [0, 1] | Name and version of the tool used to compute the aerodynamic performance |
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. |
cfx | [0, 1] | stringArrayBaseType |
cfy | [0, 1] | stringArrayBaseType |
cfz | [0, 1] | stringArrayBaseType |
cmx | [0, 1] | stringArrayBaseType |
cmy | [0, 1] | stringArrayBaseType |
cmz | [0, 1] | stringArrayBaseType |
dampingDerivatives | [0, 1] | Damping derivatives for positive and negative rotation rates |
Name | Type | Required | Description |
---|---|---|---|
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string |