aeroCaseSpecificationType

complexType · sequence

Specification

Specification of the vehicle properties and dynamics

Child elements

Name	Type	Constraints	OccurrenceHow often the element may appear at this place. The schema writes it as minOccurs and maxOccurs on the declaration.	Default	Description
sequenceThe children below must appear in exactly this order. Each may repeat as often as its own occurrence allows.
`environment`	`environmentType`		[1..1] required		Atmospheric conditions of the load case
`altitude`	`doubleBaseType`		[1..1] required		Altitude
`machNumber`	`doubleBaseType`		[1..1] required		Mach number
`angleOfSideslip`	`doubleBaseType`		[1..1] required		Angle of sideslip [deg]
choiceExactly one of the alternatives below may appear, unless the occurrence next to this line says otherwise.
`angleOfAttack`	`doubleBaseType`		[1..1] required		Angle of attack [deg]
`targetCl`	`doubleBaseType`		[1..1] required		Target lift coefficient
`pStar`	`doubleBaseType`		[0..1] optional		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`	`doubleBaseType`		[0..1] optional		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`	`doubleBaseType`		[0..1] optional		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`	`configurationType`		[0..1] optional		Configuration settings, e.g. deflections of movable devices
`weightAndBalanceUID`	`stringUIDBaseType`		[0..1] optional		Reference to a weight and balance description

Used by

In a dataset · 2 paths

In the schema · 1 declaration

Type	Name
`aeroCaseType`	`specification`