pStar Element |
Normalized roll rate [rad/sec]. It is specified around the global x-axis with the aircraft model's global reference point as origin and nondimensionalized by: pStar = p * reference length / flow speed.
Namespace: Empty
Schema: Empty
Name | Type | Required | Description |
---|---|---|---|
a | double | ||
b | double | ||
c | double | ||
delta | double | ||
externalDataDirectory | string | ||
externalDataNodePath | string | ||
externalFileName | string | ||
mu | double | ||
uncertaintyFunctionName | uncertaintyFunctionType | ||
v | double | ||
w | double |