complexType · extension complexBaseType · all
Aerodynamic performance map (rotorcraft)
Performance map with aerodynamic data. Array order is: angleOfAttack min->max then angleOfSideslip then altitude then machNumber
| Name | Type | Constraints | Use | Default | Description |
|---|---|---|---|---|---|
@externalDataDirectory | xsd:string | optional | Directory of the external data file | ||
@externalDataNodePath | xsd:string | optional | Path of the node inside the external data file | ||
@externalFileName | xsd:string | optional | Name of the external data file |
| Name | Type | Constraints | OccurrenceHow often the element may appear at this place. The schema writes it as minOccurs and maxOccurs on the declaration. | Default | Description |
|---|---|---|---|---|---|
| allThe children below may appear in any order. Each may appear at most once. | |||||
atmosphericModel | atmosphericModelOldType | [1..1] required | Atmospheric model and temperature offset | ||
machNumber | stringVectorBaseType | [1..1] required | Mach number | ||
altitude | stringVectorBaseType | [1..1] required | Altitude | ||
angleOfSideslip | stringVectorBaseType | [1..1] required | Sideslip angle | ||
angleOfAttack | stringVectorBaseType | [1..1] required | Angle of attack | ||
analysisTool | toolType | [0..1] optional | Name and version of the tool used to compute the aerodynamic performance | ||
analysisLevel | integerBaseType | [0..1] optional | 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 | stringArrayBaseType | [0..1] optional | Force coefficient in x-direction of the CPACS coordinate system | ||
cfy | stringArrayBaseType | [0..1] optional | Force coefficient in y-direction of the CPACS coordinate system | ||
cfz | stringArrayBaseType | [0..1] optional | Force coefficient in z-direction of the CPACS coordinate system | ||
cmx | stringArrayBaseType | [0..1] optional | Moment coefficient around the x-axis of the CPACS coordinate system | ||
cmy | stringArrayBaseType | [0..1] optional | Moment coefficient around the y-axis of the CPACS coordinate system | ||
cmz | stringArrayBaseType | [0..1] optional | Moment coefficient around the z-axis of the CPACS coordinate system | ||
dampingDerivatives | dampingDerivativesRatesArrayType | [0..1] optional | Damping derivatives for positive and negative rotation rates | ||
cpacs/vehicles/rotorcraft/model/analyses/aeroPerformance/globalAeroPerformance/aeroPerformanceMaps/aeroPerformanceMapcpacs/vehicles/rotorcraft/model/analyses/aeroPerformance/fuselagesAeroPerformance/fuselageAeroPerformance/aeroPerformanceMaps/aeroPerformanceMapcpacs/vehicles/rotorcraft/model/analyses/aeroPerformance/wingsAeroPerformance/wingAeroPerformance/aeroPerformanceMaps/aeroPerformanceMapcpacs/vehicles/rotorcraft/model/analyses/aeroPerformance/airfoilsAeroPerformance/airfoilAeroPerformance/aeroPerformanceMaps/aeroPerformanceMap| Type | Name |
|---|---|
aeroPerformanceMapsRCType | aeroPerformanceMap |