- a0() - Method in class jahuwaldt.aero.StdAtmos
-
Returns the standard sea level speed of sound for this
atmosphere model.
- a0() - Method in class jahuwaldt.aero.StdAtmos1962
-
Returns the standard sea level speed of sound for this
atmosphere model.
- a0() - Method in class jahuwaldt.aero.StdAtmos1976
-
Returns the standard sea level speed of sound for this
atmosphere model.
- a_a0_fn_theta(double) - Static method in class jahuwaldt.aero.Airspeeds
-
Calculates the ratio of the speed of sound to the standard sea level speed of sound
as a function of the temperature ratio.
- A_Astar(double, double) - Static method in class jahuwaldt.aero.Isentropic
-
Calculates the duct area ratio (A/A*) necessary to create sonic flow (M=1) at the
throat of the duct.
- a_fn_VT_M(double, double) - Static method in class jahuwaldt.aero.Airspeeds
-
Calculates the speed of sound as a function of the true airspeed and Mach number.
- add(AeroCoefficients) - Method in class jahuwaldt.aero.AeroCoefficients
-
Add the given aero coefficients to those contained in this
object.
- add(AeroCoefficients) - Method in class jahuwaldt.aero.AeroCoefXAft
-
Add the given aero coefficients to those contained in this
object.
- add(AeroCoefXAft) - Method in class jahuwaldt.aero.AeroCoefXAft
-
Add the given aero coefficients to those contained in this
object.
- add(int, Object) - Method in class jahuwaldt.aero.panelgeom.GeomComponent
-
Inserts the specified network at the specified position in this
component.
- add(int, Object) - Method in class jahuwaldt.aero.panelgeom.GeomConfig
-
Inserts the specified vehicle at the specified position in this configuration.
- add(int, Object) - Method in class jahuwaldt.aero.panelgeom.GeomVehicle
-
Inserts the specified component at the specified position in this vehicle.
- addAllNotes(String[]) - Method in class jahuwaldt.tools.tables.FloatTable
-
Add all the notes in an array of Strings to the list of
notes associated with this table.
- addAllNotes(String[]) - Method in class jahuwaldt.tools.tables.FTableDatabase
-
Add all the notes in an array of Strings to the list of
notes associated with this table database.
- addCA(double) - Method in class jahuwaldt.aero.AeroCoefficients
-
Add the given increment to the current value of the body
axis axial force coefficient.
- addClb(double) - Method in class jahuwaldt.aero.AeroCoefficients
-
Add the given increment to the current value of the
body axis rolling moment coefficient.
- addCMb(double) - Method in class jahuwaldt.aero.AeroCoefficients
-
Add the given increment to the current value of the
body axis pitching moment coefficient.
- addCN(double) - Method in class jahuwaldt.aero.AeroCoefficients
-
Add the given increment to the current value of the body
axis normal force coefficient.
- addCnb(double) - Method in class jahuwaldt.aero.AeroCoefficients
-
Add the given increment to the current value of the
body axis yawing moment coefficient.
- addCYb(double) - Method in class jahuwaldt.aero.AeroCoefficients
-
Add the given increment to the current value of the body
axis side force coefficient.
- addNote(String) - Method in class jahuwaldt.tools.tables.FloatTable
-
Add a new note String to the list of notes associated with
this table.
- addNote(String) - Method in class jahuwaldt.tools.tables.FTableDatabase
-
Add a new note String to the list of notes associated with
this table database.
- addSpaces(int, StringBuffer) - Static method in class jahuwaldt.tools.tables.TRUtils
-
Method that adds spaces to the start of the formatted number
(or any other string actually) until the string reaches the
specified length.
- Aero3DOF - Interface in jahuwaldt.aero
-
Interface in common to all 3-DOF static aerodynamics models.
- Aero3DOFTabular - Class in jahuwaldt.aero
-
A 3DOF aerodynamic model that makes use of data tabulated as a function of angle of
attack and Mach number.
- Aero3DOFTabular(FloatTable, FloatTable, FloatTable, String, String) - Constructor for class jahuwaldt.aero.Aero3DOFTabular
-
Construct a tabular 3-DOF aerodynamics model.
- Aero3DOFTabularGE - Class in jahuwaldt.aero
-
A 3DOF aerodynamic model that makes use of data tabulated as a function of angle of
attack and Mach number.
- Aero3DOFTabularGE(FloatTable, FloatTable, FloatTable, String, String, FloatTable, FloatTable, FloatTable, String, String) - Constructor for class jahuwaldt.aero.Aero3DOFTabularGE
-
Construct a tabular 3-DOF aerodynamics model with an increment based ground effect
model.
- AeroCoefficients - Class in jahuwaldt.aero
-
A container for aerodynamic dimensionless coefficients such as lift coefficient (CL),
drag coefficient (CD), etc.
- AeroCoefficients() - Constructor for class jahuwaldt.aero.AeroCoefficients
-
Creates an AeroCoefficients object with all the coefficients
set to zero and with no reference quantities defined.
- AeroCoefficients(AeroReference) - Constructor for class jahuwaldt.aero.AeroCoefficients
-
Creates an AeroCoefficients object with all the coefficients
set to zero and the aero reference quantities set to
the given values.
- AeroCoefficients(AeroReference, double, double, double, double, double, double) - Constructor for class jahuwaldt.aero.AeroCoefficients
-
Creates an AeroCoefficients object with the coefficients
and reference quantities as specified.
- AeroCoefXAft - Class in jahuwaldt.aero
-
A container for aerodynamic dimensionless coefficients such as lift coefficient
(CL), drag coefficient (CD), etc.
- AeroCoefXAft() - Constructor for class jahuwaldt.aero.AeroCoefXAft
-
Creates an AeroCoefXAft object with all the coefficients
set to zero and no reference quantities defined.
- AeroCoefXAft(AeroReference) - Constructor for class jahuwaldt.aero.AeroCoefXAft
-
Creates an AeroCoefXAft object with all the coefficients
set to zero and the aero reference quantities set to
the given values.
- AeroCoefXAft(AeroReference, double, double, double, double, double, double) - Constructor for class jahuwaldt.aero.AeroCoefXAft
-
Creates an AeroCoefXAft object with the body axis coefficients
and reference quantities as specified.
- AeroMethods - Class in jahuwaldt.aero
-
A set of utility methods for calculating various
aerodynamic analysis related properties.
- AeroReference - Class in jahuwaldt.aero
-
Class that serves as a container for aerodynamic reference quantities such as reference
area, span, chord length, and moment reference center.
- AeroReference(double, Unit<Area>, double, double, double, double, double, Unit<Length>) - Constructor for class jahuwaldt.aero.AeroReference
-
Creates an AeroReference object with the given reference quantities and units.
- Airfoil - Interface in jahuwaldt.aero.airfoils
-
Defines the interface in common to all airfoil type objects.
- Airspeeds - Class in jahuwaldt.aero
-
A collection of static routines for calculating various airspeeds.
- Airspeeds() - Constructor for class jahuwaldt.aero.Airspeeds
-
- alpha - Variable in class jahuwaldt.aero.AeroCoefficients
-
Flow angles used to transform between axis systems.
- alt - Variable in class jahuwaldt.aero.StdAtmos
-
- arraycopy(float[], int, FloatArrayNDim, int[], int) - Static method in class jahuwaldt.tools.tables.FloatArrayNDim
-
Copy a given Java array into a FloatArrayNDim array.
- arraycopy(FloatArrayNDim, int[], float[], int, int) - Static method in class jahuwaldt.tools.tables.FloatArrayNDim
-
Copy a given FloatArrayNDim array into a Java array.