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 HierarchySystemObject
AGI.Foundation.InfrastructureDefinitionalObject
AGI.Foundation.AircraftPropagationSimpleFixedWingForwardFlightAerodynamics
AGI.Foundation.InfrastructureDefinitionalObject
AGI.Foundation.AircraftPropagationSimpleFixedWingForwardFlightAerodynamics
Namespace: AGI.Foundation.AircraftPropagation
Assembly: AGI.Foundation.AircraftPropagation (in AGI.Foundation.AircraftPropagation.dll) Version: 24.3.420.0 (24.3.420.0)
SyntaxThe SimpleFixedWingForwardFlightAerodynamics type exposes the following members.
Constructors| Name | Description | |
|---|---|---|
 | SimpleFixedWingForwardFlightAerodynamics | Initializes a new instance. |
| SimpleFixedWingForwardFlightAerodynamics(SimpleFixedWingForwardFlightAerodynamics, CopyContext) | Initializes a new instance as a copy of an existing instance. |
Properties| Name | Description | |
|---|---|---|
 | AngleOfAttack |
Gets or sets a Scalar which provides the value of the angle of attack.
|
| AspectRatio |
Gets or sets the aspect ratio of the wing.
|
| DragCoefficientAtMinimum |
Gets or sets the minimum drag coefficient value.
|
| DragIndex |
Gets or sets the drag index.
|
| DynamicPressure |
Gets or sets a Scalar which provides the value of the dynamic pressure.
|
| IsFrozen |
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.) |
| LiftCoefficientAtZeroAngleOfAttack |
Gets or sets the lift coefficient value at zero angle of attack.
|
| LiftCoefficientSlope |
Gets or sets the lift coefficient slope with respect to the angle of attack in units of radians-1.
|
| OswaldEfficiencyFactor |
Gets or sets the Oswald efficiency factor for the wing.
|
| ReferenceArea |
Gets or sets the reference area of the wing.
|
Methods| Name | Description | |
|---|---|---|
| Clone |
Clones this object using the specified context.
(Overrides DefinitionalObjectClone(CopyContext).) |
 | ComputeDragCoefficient |
Computes the drag coefficient from the provided parameters.
|
| ComputeLiftCoefficient |
Computes the lift coefficient from the provided parameters.
|
| EnumerateDependencies |
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).) |
| Equals | Determines whether the specified object is equal to the current object. (Inherited from Object.) |
| Freeze |
Freezes this object. Further attempts to modify it will result
in an ObjectFrozenException.
(Inherited from DefinitionalObject.) |
| GetDefinitionHashCode |
Gets a hash code representing the definition of this object.
(Inherited from DefinitionalObject.) |
| GetEvaluator |
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.
|
| GetEvaluator(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.
|
| GetHashCode | Serves as the default hash function. (Inherited from Object.) |
| GetType | Gets the Type of the current instance. (Inherited from Object.) |
| IsSameDefinition |
Determines if this object has the same definition as another object.
(Inherited from DefinitionalObject.) |
| ToString | Returns a string that represents the current object. (Inherited from Object.) |
See Also