aeroCaseSpecificationType Complex Type |
Specification
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
Sequence | ||
environment | Environmental conditions | |
altitude | Altitude | |
machNumber | Mach number | |
angleOfSideslip | Angle of sideslip [deg] | |
Choice | ||
angleOfAttack | Angle of attack [deg] | |
targetCl | Target lift coefficient | |
pStar | [0, 1] | 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. |
qStar | [0, 1] | Normalized pitch rate [rad/sec]. It is specified around the global y-axis with the aircraft model's global reference point as origin and nondimensionalized by: qStar = q * reference length / flow speed. |
rStar | [0, 1] | Normalized yaw rate [rad/sec]. It is specified around the global z-axis with the aircraft model's global reference point as origin and nondimensionalized by: rStar = r * reference length / flow speed. |
configuration | [0, 1] | Configuration |
weightAndBalanceUID | [0, 1] | Reference to a weight and balance description |