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SimpleFixedWingForwardFlightAerodynamics Class

Defines an aerodynamic model for fixed wing aircraft under nominal forward flight conditions which accounts for lift and drag forces but assumes that the slip (or side) force is zero, by definition.
Inheritance Hierarchy
SystemObject
  AGI.Foundation.InfrastructureDefinitionalObject
    AGI.Foundation.AircraftPropagationSimpleFixedWingForwardFlightAerodynamics

Namespace:  AGI.Foundation.AircraftPropagation
Assembly:  AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 19.1.398.0 (19.1.398.0)
Syntax
public sealed class SimpleFixedWingForwardFlightAerodynamics : DefinitionalObject

The SimpleFixedWingForwardFlightAerodynamics type exposes the following members.

Constructors
Properties
  NameDescription
Public propertyAngleOfAttack
Gets or sets a Scalar which provides the value of the angle of attack.
Public propertyAspectRatio
Gets or sets the aspect ratio of the wing.
Public propertyDragCoefficientAtMinimum
Gets or sets the minimum drag coefficient value.
Public propertyDragIndex
Gets or sets the drag index.
Public propertyDynamicPressure
Gets or sets a Scalar which provides the value of the dynamic pressure.
Public propertyIsFrozen
Gets a value indicating whether this object is frozen. A frozen object cannot be modified and an ObjectFrozenException will be thrown if an attempt is made to do so.
(Inherited from DefinitionalObject.)
Public propertyLiftCoefficientAtZeroAngleOfAttack
Gets or sets the lift coefficient value at zero angle of attack.
Public propertyLiftCoefficientSlope
Gets or sets the lift coefficient slope with respect to the angle of attack in units of radians-1.
Public propertyOswaldEfficiencyFactor
Gets or sets the Oswald efficiency factor for the wing.
Public propertyReferenceArea
Gets or sets the reference area of the wing.
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Methods
  NameDescription
Public methodClone
Clones this object using the specified context.
(Overrides DefinitionalObjectClone(CopyContext).)
Public methodStatic memberComputeDragCoefficient
Computes the drag coefficient from the provided parameters.
Public methodStatic memberComputeLiftCoefficient
Computes the lift coefficient from the provided parameters.
Public methodEnumerateDependencies
Enumerates the dependencies of this object by calling EnumerateT(T) for each object that this object directly depends upon. Derived classes which contain additional dependencies MUST override this method, call the base implementation, and enumerate dependencies introduced by the derived class.
(Overrides DefinitionalObjectEnumerateDependencies(DependencyEnumerator).)
Public methodEquals
Determines whether the specified object is equal to the current object.
(Inherited from Object.)
Public methodFreeze
Freezes this object. Further attempts to modify it will result in an ObjectFrozenException.
(Inherited from DefinitionalObject.)
Public methodGetDefinitionHashCode
Gets a hash code representing the definition of this object.
(Inherited from DefinitionalObject.)
Public methodGetEvaluator
Gets an evaluator that computes the aerodynamic force in the wind frame as drag, side, and lift force components. The side force is zero, by definition, for this aerodynamic model.
Public methodGetEvaluator(EvaluatorGroup)
Gets an evaluator that computes the aerodynamic force in the wind frame as drag, side, and lift force components. The side force is zero, by definition, for this aerodynamic model.
Public methodGetHashCode
Serves as the default hash function.
(Inherited from Object.)
Public methodGetType
Gets the Type of the current instance.
(Inherited from Object.)
Public methodIsSameDefinition
Determines if this object has the same definition as another object.
(Inherited from DefinitionalObject.)
Public methodToString
Returns a string that represents the current object.
(Inherited from Object.)
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See Also