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S

scale(double, double, double) - Method in interface jahuwaldt.aero.panelgeom.GeomElement
Scale this element by the given scale factor in each axis direction.
scale(double, double, double) - Method in class jahuwaldt.aero.panelgeom.GeomElementList
Scale this element by the given scale factor in each axis direction.
scale(double, double, double) - Method in class jahuwaldt.aero.panelgeom.GeomNetwork
Scale this network by a specified factor along each axis.
scale(double, double, double) - Method in class jahuwaldt.aero.panelgeom.GeomPanel
Scale this panel by the given factor along each axis.
scale(double, double, double) - Method in class jahuwaldt.aero.panelgeom.GeomPoint
Scale this point by a specified factor along each axis.
set(int, Object) - Method in class jahuwaldt.aero.panelgeom.GeomComponent
Replaces the network at the specified position in this component with the specified network.
set(int, Object) - Method in class jahuwaldt.aero.panelgeom.GeomConfig
Replaces the vehicle at the specified position in this configuration with the specified vehicle.
set(int, Object) - Method in class jahuwaldt.aero.panelgeom.GeomVehicle
Replaces the component at the specified position in this vehicle with the specified component.
set(int[], float) - Method in class jahuwaldt.tools.tables.FloatArrayNDim
Set the value of a particular element in the n dimensional array.
set(int, float) - Method in class jahuwaldt.tools.tables.FloatArrayNDim
Set the value of a particular element in the 1-dimensional array.
set(int[], float) - Method in class jahuwaldt.tools.tables.FloatTable
Set the value of a particular element in the table.
setAll(float) - Method in class jahuwaldt.tools.tables.FloatArrayNDim
Set all the values stored in this array to the given value.
setAltitude(double) - Method in class jahuwaldt.aero.StdAtmos
Sets the geometric altitude where the standard atmosphere is to be calculated.
setAltitude(double) - Method in class jahuwaldt.aero.StdAtmos1962
Sets the geometric altitude where the standard atmosphere is to be calculated.
setAltitude(double) - Method in class jahuwaldt.aero.StdAtmos1976
Sets the geometric altitude where the standard atmosphere is to be calculated.
setAngles(double, double, double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the free stream flow angles used to resolve body axis coefficients to wind and stability axes and vis-versa.
setAOA(float) - Method in interface jahuwaldt.aero.Aero3DOF
Method that sets the angle of attack in degrees.
setAOA(float) - Method in class jahuwaldt.aero.Aero3DOFTabular
Method that sets the angle of attack in degrees.
setAOA(float) - Method in class jahuwaldt.aero.Aero3DOFTabularGE
Method that sets the angle of attack.
setAOA(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the angle of attack used for resolving body axis coefficients to wind and stability axes and back again.
setAOA(float) - Method in interface jahuwaldt.aero.ControlAero3DOF
Method that sets the angle of attack in degrees.
setAOA(float) - Method in class jahuwaldt.aero.ControlAero3DOFTabular
Method that sets the angle of attack in degrees.
setAOA(float) - Method in interface jahuwaldt.aero.ControlHingeMoments
Method that sets the angle of attack in degrees.
setAOA(float) - Method in class jahuwaldt.aero.ControlHMLinearizedTabular
Method that sets the angle of attack in degrees.
setBodyAxesForces(double, double, double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the body axis force coefficients.
setBodyAxesMoments(double, double, double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the body axis moment coefficients.
setBreakpoint(int, int, float) - Method in class jahuwaldt.tools.tables.FloatTable
Set the value of a particular table breakpoint.
setBreakpoints(int, float[]) - Method in class jahuwaldt.tools.tables.FloatTable
Sets the array of breakpoints corresponding to the specified dimension (independent variable).
setCA(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the body axis axial force coefficient.
setClb(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the body axis rolling moment coefficient.
setCMb(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the body axis pitching moment coefficient.
setCN(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the body axis normal force coefficient.
setCnb(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the body axis yawing moment coefficient.
setCYb(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the body axis side force coefficient.
setDef(float) - Method in interface jahuwaldt.aero.ControlAero3DOF
Sets the control deflection angle in degrees
setDef(float) - Method in class jahuwaldt.aero.ControlAero3DOFTabular
Sets the control deflection angle in degrees.
setDef(float) - Method in interface jahuwaldt.aero.ControlHingeMoments
Sets the control deflection angle in degrees.
setDef(float) - Method in class jahuwaldt.aero.ControlHMLinearizedTabular
Sets the control deflection angle in degrees.
setFileUnits(Unit<Length>) - Method in interface jahuwaldt.aero.panelgeom.GeomReader
Method provided by sub-classes that specified the units used for the geometry as stored in the disk file.
setFileUnits(Unit<Length>) - Method in class jahuwaldt.aero.panelgeom.GGPGeomReader
Method that specifies the units used for the geometry as stored in the file.
setFileUnits(Unit<Length>) - Method in class jahuwaldt.aero.panelgeom.POIGeomReader
Method that specifies the units used for the geometry as stored in the POI file.
setGamma(double) - Method in class jahuwaldt.aero.ConicalShock
Method used to set the specific heat ratio for the gas used in the calculation of the conical shock properties.
setHOB(float) - Method in interface jahuwaldt.aero.Aero3DOF
Sets the height above ground level (for ground effect modeling).
setHOB(float) - Method in class jahuwaldt.aero.Aero3DOFTabular
Sets the height above ground level (for ground effect modeling).
setHOB(float) - Method in class jahuwaldt.aero.Aero3DOFTabularGE
Sets the height above ground level (for ground effect modeling).
setHOB(float) - Method in interface jahuwaldt.aero.ControlAero3DOF
Sets the height above ground level (for ground effect modeling).
setHOB(float) - Method in class jahuwaldt.aero.ControlAero3DOFTabular
Sets the height above ground level (for ground effect modeling).
setHOB(float) - Method in interface jahuwaldt.aero.ControlHingeMoments
Sets the height above ground level (for ground effect modeling).
setHOB(float) - Method in class jahuwaldt.aero.ControlHMLinearizedTabular
Sets the height above ground level (for ground effect modeling).
setIndepName(int, String) - Method in class jahuwaldt.tools.tables.FloatTable
Set the name of the specified independent variable.
setIndepNames(String[]) - Method in class jahuwaldt.tools.tables.FloatTable
Sets the names of the independent variables to those in the given array.
setMach(float) - Method in interface jahuwaldt.aero.Aero3DOF
Method that sets the Mach number.
setMach(float) - Method in class jahuwaldt.aero.Aero3DOFTabular
Method that sets the Mach number.
setMach(float) - Method in interface jahuwaldt.aero.ControlAero3DOF
Method that sets the Mach number.
setMach(float) - Method in class jahuwaldt.aero.ControlAero3DOFTabular
Method that sets the Mach number.
setMach(float) - Method in interface jahuwaldt.aero.ControlHingeMoments
Method that sets the Mach number.
setMach(float) - Method in class jahuwaldt.aero.ControlHMLinearizedTabular
Method that sets the Mach number.
setMaximumFractionDigits(int) - Method in class jahuwaldt.util.ExponentialFormat
Sets the maximum number of digits allowed in the fraction portion of a number.
setMinimumExponentDigits(int) - Method in class jahuwaldt.util.ExponentialFormat
Set the minimum number of digits to use for the exponent when formatting a number.
setMinimumFractionDigits(int) - Method in class jahuwaldt.util.ExponentialFormat
Sets the minimum number of digits allowed in the fraction portion of a number.
setName(String) - Method in interface jahuwaldt.aero.panelgeom.GeomElement
Change the name of this geometry element.
setName(String) - Method in class jahuwaldt.aero.panelgeom.GeomElementList
Change the name of this geometry element.
setName(String) - Method in class jahuwaldt.aero.panelgeom.GeomNetwork
Change the name of this network.
setRoll(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the roll angle used for resolving body axis coefficients to wind and stability axes and back again.
setRoundingMode(RoundingMode) - Method in class jahuwaldt.util.ExponentialFormat
Sets the RoundingMode used in this NumberFormat.
setSideslip(double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the sideslip angle used for resolving body axis coefficients to wind and stability axes and back again.
setStabilityAxesForces(double, double, double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the stability axis force coefficients.
setStabilityAxesMoments(double, double, double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the stability axis moment coefficients.
setTableName(String) - Method in class jahuwaldt.tools.tables.FloatTable
Sets this table's name to the specified String.
setWindAxesForces(double, double, double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the wind axis force coefficients.
setWindAxesMoments(double, double, double) - Method in class jahuwaldt.aero.AeroCoefficients
Set the wind axis moment coefficients.
setX(double) - Method in class jahuwaldt.aero.panelgeom.GeomPoint
Set the X-coordinate of the point.
setY(double) - Method in class jahuwaldt.aero.panelgeom.GeomPoint
Set the Y-coordinate of the point.
setZ(double) - Method in class jahuwaldt.aero.panelgeom.GeomPoint
Set the Z-coordinate of the point.
seval(int, double, double[], double[], double[], double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA6Series
Evaluate the cubic spline function.
shockAngle(double, double, boolean) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the oblique shock wave angle given the cone half-angle and the Mach number upstream of the oblique shock.
ShockBetaEvaluator - Class in jahuwaldt.aero
Used by ShockMethods.os_beta() and a root solver to iteratively determine beta.
ShockBetaEvaluator() - Constructor for class jahuwaldt.aero.ShockBetaEvaluator
 
ShockMachEvaluator - Class in jahuwaldt.aero
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.
ShockMachEvaluator() - Constructor for class jahuwaldt.aero.ShockMachEvaluator
 
ShockMachNuEvaluator - Class in jahuwaldt.aero
Used by ShockMethods.pm_Mach() and a root solver to iteratively determine Mach number for a given Prandtl-Meyer function value.
ShockMachNuEvaluator() - Constructor for class jahuwaldt.aero.ShockMachNuEvaluator
 
ShockMethods - Class in jahuwaldt.aero
A set of utility methods for calculating the properties across shock waves.
sigma - Variable in class jahuwaldt.aero.StdAtmos
 
size() - Method in class jahuwaldt.aero.panelgeom.GeomElementList
Returns the number of sub-elements in this geometry element.
size() - Method in class jahuwaldt.tools.tables.FloatArrayNDim
Returns the overall number of elements in the array.
size() - Method in class jahuwaldt.tools.tables.FloatTable
Returns the total number of elements in the dependent data for this table.
size() - Method in class jahuwaldt.tools.tables.FTableDatabase
Returns the number of tables in this table database.
sizes - Variable in class jahuwaldt.tools.tables.FloatArrayNDim
The number of elements per dimension.
spline(int, double[], double[], double[], double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA6Series
Compute the coefficients of a cubic spline NOTES - From "Computer Methods for Mathematical Computations", by Forsythe, Malcolm, and Moser.
StdAtmos - Class in jahuwaldt.aero
An abstract class that provides standard functionality for all atmosphere models that sub-class off of this one.
StdAtmos() - Constructor for class jahuwaldt.aero.StdAtmos
 
StdAtmos1962 - Class in jahuwaldt.aero
This class provides methods for calculating the atmospheric properties of the U.S.
StdAtmos1962() - Constructor for class jahuwaldt.aero.StdAtmos1962
Constructor that assumes an altitude of 0 meters,
StdAtmos1962(double) - Constructor for class jahuwaldt.aero.StdAtmos1962
Constructor taking a value of geometric altitude in meters.
StdAtmos1976 - Class in jahuwaldt.aero
This class provides methods for calculating the atmospheric properties of the ICAO 1976 Standard Atmosphere to an arbitrary altitude (above 3280839.9 ft the values are constant).
StdAtmos1976() - Constructor for class jahuwaldt.aero.StdAtmos1976
Constructor that assumes an altitude of 0 meters,
StdAtmos1976(double) - Constructor for class jahuwaldt.aero.StdAtmos1976
Constructor that takes a value of altitude in meters.
STRONG - Static variable in class jahuwaldt.aero.ConicalShock
Constant indicating that a strong shock solution should be returned from shockAngle().
STRONG - Static variable in class jahuwaldt.aero.ShockMethods
Constant indicating that a strong shock solution should be returned from os_beta().
subElements - Variable in class jahuwaldt.aero.panelgeom.GeomElementList
Array of sub-elements.
SUBSONIC - Static variable in class jahuwaldt.aero.Isentropic
Constant indicating that a subsonic solution should be returned in Me().
subtract(AeroCoefficients) - Method in class jahuwaldt.aero.AeroCoefficients
Subtract the given aero coefficients from those contained in object.
subtract(AeroCoefficients) - Method in class jahuwaldt.aero.AeroCoefXAft
Subtract the given aero coefficients from those contained in this object.
subtract(AeroCoefXAft) - Method in class jahuwaldt.aero.AeroCoefXAft
Subtract the given aero coefficients from those contained in this object.
SUPERSONIC - Static variable in class jahuwaldt.aero.Isentropic
Constant indicating that a supersonic solution should be returned in Me().
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