| aeroFuseQuasiSteadyRotationType Complex Type |
aeroFuseQuasiSteadyRotationType
Namespace: Empty
Schema: Empty
Base Type
UsagesChildren| 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 |
RemarksaeroFuseQuasiSteadyRotationType, contain the normalized
roll, pitch and yaw rate. In loadcase, the calculation of
quasi-steady rotation can be performed at the given roll, pitch
and yaw rate. In polarcasse, the damping derivatives can be
obtained by performing quasi-steady rotation calculations at
given roll rate, pitch rate and yaw rate respectively.