aeroLandingGearType
Namespace: Empty
Schema: Empty
Type Parents Children Name | Occurrences | Description |
---|
Sequence | | |
landingGearUID | | Reference to the landingGear
|
relDeflection | | Relative deflection of the landing gear
|
dcd | [0, 1] | Delta drag coefficient for landing gear
|
dcs | [0, 1] | Delta coefficient for landing gear side force (perpendicular to lift and drag)
|
dcl | [0, 1] | Delta lift coefficient for landing gear
|
dcmd | [0, 1] | Delta moment coefficient around drag axis
|
dcms | [0, 1] | Delta moment coefficient around side force axis (perpendicular to lift and drag)
|
dcml | [0, 1] | Delta moment coefficient around lift axis
|
Attributes LandingGearPerformanceMap type, containing a delta
perfomance map with aerodynamic data for a landing gear. This
means that the coefficients are deltas to be added to the
corresponding coefficients of the base performance map. Array
order is (from innermost to outermost loop): relativeDeflection
min->max, then angleOfAttack, then angleOfSideslip, then
altitude, then machNumber. AngleOfAttack, angleOfSideslip,
altitude and machNumber are taken from the basic performance map
one level above. For the definition of the coefficients,
please refer to the description of the base performance mapLandingGearPerformanceMap type, containing a delta
perfomance map with aerodynamic data for a landing gear. This
means that the coefficients are deltas to be added to the
corresponding coefficients of the base performance map for a
specific landing gear deflection. Array order is (from innermost
to outermost loop): relativeDeflection min->max, then
angleOfAttack, then angleOfSideslip, then altitude, then
machNumber. AngleOfAttack, angleOfSideslip, altitude
and machNumber are taken from the base performance map
one level above. For the definition of the coefficients,
please refer to the description of the base performance map
See Also