📄 aspectratiocalc.desc
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MDOLVersion: 6.0
CompilerOptions: warn
Task Airplane
TaskHeader Airplane
Version: 1.0
Evaluation: taskplan
ControlMode: user
RunCounter: 1
BoundsPolicy: adjustvalue
CheckPoint: unknown
RandGenInit: default
End TaskHeader Airplane
Inputs Airplane
Parameter: WingSpan Type: real InitialValue: 22.72
Parameter: WingArea Type: real InitialValue: 0
End Inputs Airplane
Outputs Airplane
Parameter: AR Type: real
Parameter: WingChord Type: real
End Outputs Airplane
Calculations Airplane
Calculation AspectRatioCalc
Parameters
WingSpan WingArea AR WingChord
Tcl
set AR(V) [expr $WingSpan(V)*$WingSpan(V)/$WingArea(V)]
set WingChord(V) [expr $WingArea(V)/$WingSpan(V)]
End Tcl
End Calculation AspectRatioCalc
End Calculations Airplane
TaskProcess Airplane
Control: [
AspectRatioCalc
]
End TaskProcess Airplane
Optimization Airplane
PotentialVariables:
WingSpan WingArea
Variables:
WingSpan WingArea
VariableScaling
Parameter: WingSpan ScaleFactor: 1.0
Parameter: WingArea ScaleFactor: 1.0
InputConstraints
PotentialObjectives:
WingSpan WingArea AR WingChord
OutputConstraints
End Optimization Airplane
DataStorage Airplane
Restore: no
DataLog: "Airplane.db" Mode: overwrite
Levels: all
StoreGradRuns: yes
StoreApproxRuns: yes
End DataStorage Airplane
End Task Airplane
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