| quasiSteadyRotation Element |
aeroFuseQuasiSteadyRotationType, contain the normalized roll, pitch and yaw rate for quasi-steady rotation calculation in loadcase or for damping derivatives calculation in polarcase.
Namespace: Empty
Schema: Empty
Type
ParentsChildren| Name | Occurrences | Description |
|---|---|---|
 All | ||
 pitchRate | [0, 1] | normalized pitch rate, default = 0.01. The pitch rate and pitching moment coefficient are normalized by lengthCMY. |
| rollRate | [0, 1] | normalized roll rate, default = 0.01. The roll rate is nondimensionalized by 2*lengthCMX, but the rolling moment coefficient is normalized by lengthCMX. |
| yawRate | [0, 1] | normalized yaw rate, default = 0.01. The yaw rate is nondimensionalized by 2*lengthCMX, but the yawing moment coefficient is normalized by lengthCMX. |
Attributes| Name | Type | Required | Description |
|---|---|---|---|
 externalDataDirectory |  string | ||
| externalDataNodePath | string | ||
| externalFileName | string |
See Also