Package | Description |
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jahuwaldt.aero |
Class and Description |
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Aero3DOF
Interface in common to all 3-DOF static aerodynamics models.
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Aero3DOFTabular
A 3DOF aerodynamic model that makes use of data tabulated as a function of angle of
attack and Mach number.
|
AeroCoefficients
A container for aerodynamic dimensionless coefficients such as lift coefficient (CL),
drag coefficient (CD), etc.
|
AeroCoefXAft
A container for aerodynamic dimensionless coefficients such as lift coefficient
(CL), drag coefficient (CD), etc.
|
AeroReference
Class that serves as a container for aerodynamic reference quantities such as reference
area, span, chord length, and moment reference center.
|
ControlAero3DOF
Interface in common to all 3-DOF static flight control aerodynamics models.
|
ControlHingeMoments
Interface in common to all aerodynamic flight control hinge-moment models.
|
IsentropicMeEvaluator
Used by Isentropic.Me() and a root solver to iteratively determine the local Mach
number at the entrance or exit of a duct with a sonic condition at the throat.
|
ShockBetaEvaluator
Used by ShockMethods.os_beta() and a root solver to iteratively determine beta.
|
ShockMachEvaluator
Used by ShockMethods.os_mach() and a root solver to iteratively determine Mach number
for an oblique shock when given the incline and shock angles.
|
ShockMachNuEvaluator
Used by ShockMethods.pm_Mach() and a root solver to iteratively determine Mach number
for a given Prandtl-Meyer function value.
|
StdAtmos
An abstract class that provides standard functionality
for all atmosphere models that sub-class off of this
one.
|