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A

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.
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