aeroCaseSpecificationType Complex Type |
Specification
Namespace: Empty
Schema: Empty
Name | Occurrences | Description |
---|---|---|
![]() | ||
![]() | Environmental conditions | |
![]() | Altitude | |
![]() | Mach number | |
![]() | Angle of sideslip [deg] | |
![]() | ||
![]() | Angle of attack [deg] | |
![]() | Target lift coefficient | |
![]() | [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. |
![]() | [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. |
![]() | [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. |
![]() | [0, 1] | Configuration |
![]() | [0, 1] | Reference to a weight and balance description |