Package | Description |
---|---|
fr.cnes.sirius.patrius.assembly | |
fr.cnes.sirius.patrius.assembly.models.aerocoeffs | |
fr.cnes.sirius.patrius.assembly.vehicle |
Modifier and Type | Method and Description |
---|---|
void |
Vehicle.setAerodynamicsProperties(AerodynamicCoefficient cx,
AerodynamicCoefficient cz)
Set aerodynamics properties only if possible : main shape must be a sphere or there must be
no solar panels.
|
Modifier and Type | Class and Description |
---|---|
class |
AbstractAeroCoeff1D
Aerodynamic coefficient function of one variable.
|
class |
AeroCoeffByAltitude
Aerodynamic coefficient function of the spacecraft altitude.
|
class |
AeroCoeffByAoA
Aerodynamic coefficient function of the spacecraft angle of attack.
|
class |
AeroCoeffByAoAAndMach
Aerodynamic coefficient function of the spacecraft angle of attack and Mach number.
|
class |
AeroCoeffByMach
Aerodynamic coefficient function of the spacecraft Mach number.
|
class |
AeroCoeffConstant
Constant aerodynamic coefficient.
|
Modifier and Type | Method and Description |
---|---|
AerodynamicCoefficient |
AerodynamicProperties.getDragCoef()
Get the drag coefficient.
|
AerodynamicCoefficient |
AerodynamicProperties.getLiftCoef()
Get the lift coefficient.
|
Constructor and Description |
---|
AerodynamicProperties(Sphere sphere,
AerodynamicCoefficient dragCoefIn,
AerodynamicCoefficient liftCoefIn)
Constructor.
|
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