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C

C81Reader - Class in jahuwaldt.tools.tables
A class that provides a method for reading C-81 airfoil aerodynamics data tables.
C81Reader() - Constructor for class jahuwaldt.tools.tables.C81Reader
 
CA - Variable in class jahuwaldt.aero.AeroCoefficients
Body axes force coefficients.
calcCamber(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4Cambered
Method to calculate the camber distribution for the airfoil.
calcCamber(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4ModCambered
Method to calculate the camber distribution for the airfoil.
calcCamber(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4Uncambered
Method to calculate the camber distribution for the airfoil.
calcCamber(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA5Cambered
Method to calculate the camber distribution for the airfoil.
calcCamber(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA5Reflexed
Method to calculate the camber distribution for the airfoil.
calcLESlope(NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4Cambered
Method to determine the local slope of the airfoil at the leading edge.
calcLESlope(NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4ModCambered
Method to determine the local slope of the airfoil at the leading edge.
calcLESlope(NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4Uncambered
Method to determine the local slope of the airfoil at the leading edge.
calcLESlope(NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA5Cambered
Method to determine the local slope of the airfoil at the leading edge.
calcLESlope(NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA5Reflexed
Method to determine the local slope of the airfoil at the leading edge.
calcOrdinateAft(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4ModUncambered
Method to calculate the ordinates of the uncambered airfoil aft of the maximum thickness point.
calcOrdinateAft(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4Uncambered
Method to calculate the ordinate of the uncambered airfoil aft of the maximum thickness point.
calcOrdinateForward(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4ModUncambered
Method to calculate the ordinates of the uncambered airfoil forward of the maximum thickness point.
calcOrdinateForward(double, NACA4Uncambered.Ordinate) - Method in class jahuwaldt.aero.airfoils.NACA4Uncambered
Method to calculate the ordinate of the uncambered airfoil forward of the maximum thickness point.
camberLine - Variable in class jahuwaldt.aero.airfoils.NACA4Uncambered
 
canReadData(String, InputStream) - Method in class jahuwaldt.tools.tables.C81Reader
Method that determines if this reader can read data from the specified input stream.
canReadData(String, InputStream) - Method in class jahuwaldt.tools.tables.CSVReader
Method that determines if this reader can read data from the specified input stream.
canReadData(String, InputStream) - Method in class jahuwaldt.tools.tables.FDAReader
Method that determines if this reader can read data from the specified input stream.
canReadData(String, InputStream) - Method in class jahuwaldt.tools.tables.FLABSavReader
Method that determines if this reader can read data from the specified input stream.
canReadData(String, InputStream) - Method in interface jahuwaldt.tools.tables.FTableReader
Method that determines if this reader can read data from the specified input stream.
canReadData(String, InputStream) - Method in class jahuwaldt.tools.tables.NASAReader
Method that determines if this reader can read data from the specified input stream.
canReadData(String, InputStream) - Method in class jahuwaldt.tools.tables.OTISTableReader
Method that determines if this reader can read data from the specified input stream.
canReadData(String, InputStream) - Method in class jahuwaldt.tools.tables.POSTTableReader
Method that determines if this reader can read data from the specified input stream.
canWriteData() - Method in class jahuwaldt.tools.tables.C81Reader
Returns false.
canWriteData() - Method in class jahuwaldt.tools.tables.CSVReader
Returns true.
canWriteData() - Method in class jahuwaldt.tools.tables.FDAReader
Returns true.
canWriteData() - Method in class jahuwaldt.tools.tables.FLABSavReader
Returns true.
canWriteData() - Method in interface jahuwaldt.tools.tables.FTableReader
Returns true if this class can write at least some data in the format supported by this class.
canWriteData() - Method in class jahuwaldt.tools.tables.NASAReader
Returns true.
canWriteData() - Method in class jahuwaldt.tools.tables.OTISTableReader
Returns true.
canWriteData() - Method in class jahuwaldt.tools.tables.POSTTableReader
Returns true.
changeAreaUnits(Unit<Area>) - Method in class jahuwaldt.aero.AeroReference
Change the current area units used by this reference object.
changeLengthUnits(Unit<Length>) - Method in class jahuwaldt.aero.AeroReference
Change the current length units used by this reference object.
changeRef(AeroReference) - Method in class jahuwaldt.aero.AeroCoefficients
Change the reference quantities used by this set of aero coefficients to those given.
changeRef(AeroReference) - Method in class jahuwaldt.aero.AeroCoefXAft
Change the reference quantities used by this set of aero coefficients to those given.
chord - Variable in class jahuwaldt.aero.airfoils.NACA4Uncambered
Chord length.
Clb - Variable in class jahuwaldt.aero.AeroCoefficients
Body axes moment coefficients.
clear() - Method in class jahuwaldt.aero.panelgeom.GeomElementList
Removes all the sub-elements from this geometry element.
clear() - Method in class jahuwaldt.tools.tables.FTableDatabase
Clear this database so that it contains no tables.
clearNotes() - Method in class jahuwaldt.tools.tables.FloatTable
Removes all notes associated with this table.
clearNotes() - Method in class jahuwaldt.tools.tables.FTableDatabase
Removes all notes associated with this table database.
clone() - Method in class jahuwaldt.aero.AeroCoefficients
Make a copy of this AeroCoefficients object.
clone() - Method in class jahuwaldt.aero.AeroReference
Make a copy of this AeroReference object.
clone() - Method in interface jahuwaldt.aero.panelgeom.GeomElement
Make a copy of this geometry element object.
clone() - Method in class jahuwaldt.aero.panelgeom.GeomElementList
Make a copy of this geometry element object.
clone() - Method in class jahuwaldt.aero.panelgeom.GeomNetwork
Make a copy of this GeomNetwork object.
clone() - Method in class jahuwaldt.aero.panelgeom.GeomPanel
Make a copy of this GeomPanel object.
clone() - Method in class jahuwaldt.aero.panelgeom.GeomPoint
Make a copy of this GeomPoint object.
clone() - Method in class jahuwaldt.tools.tables.FloatArrayNDim
Make a copy of this n-dimensional array.
clone() - Method in class jahuwaldt.tools.tables.FloatTable
Make a copy of this function table.
clone() - Method in class jahuwaldt.tools.tables.FTableDatabase
Creates a deep copy of this table database object and all the tables that it contains.
clone() - Method in class jahuwaldt.util.ExponentialFormat
Create a deep copy of this number format object.
clone() - Method in class jahuwaldt.util.GeneralFormat
Create a deep copy of this number format object.
CMb - Variable in class jahuwaldt.aero.AeroCoefficients
Body axes moment coefficients.
CN - Variable in class jahuwaldt.aero.AeroCoefficients
Body axes force coefficients.
Cnb - Variable in class jahuwaldt.aero.AeroCoefficients
Body axes moment coefficients.
compare(T, T) - Method in class jahuwaldt.util.ToStringComparator
Compares the strings returned from each Object's "toString()" method lexicographically using the String.compareTo() method.
components() - Method in class jahuwaldt.aero.panelgeom.GeomVehicle
Return an enumeration of all the components in this vehicle.
coneAngle(double, double) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the cone half-angle (thetaC) given the shock angle and the Mach number upstream of the oblique shock.
coneMach(double, double) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the Mach number at the surface of a cone in supersonic flow given the Mach number upstream of the oblique shock and the shock angle.
coneP_P0(double, double) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the ratio of static pressure at the surface of the cone to the static pressure upstream of the oblique shock forward of the cone given the free-stream Mach number and the conical shock angle.
conePT_P(double, double) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the ratio of total and static pressure at the surface of the cone given the free-stream Mach number and the conical shock angle.
coneRho_Rho0(double, double) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the ratio of static density at the surface of the cone to the static density upstream of the oblique shock forward of the cone given the free-stream Mach number and the conical shock angle.
coneRhoT_Rho(double, double) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the ratio of total and static density at the surface of the cone given the free-stream Mach number and the conical shock angle.
coneT_T0(double, double) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the ratio of static temperature at the surface of the cone to the static temperature upstream of the oblique shock forward of the cone given the free-stream Mach number and the conical shock angle.
coneTT_T(double, double) - Method in class jahuwaldt.aero.ConicalShock
Method that computes the ratio of total and static temperature at the surface of the cone given the free-stream Mach number and the conical shock angle.
ConicalShock - Class in jahuwaldt.aero
A class that computes the properties of a semi-infinite cone in supersonic flow.
ConicalShock() - Constructor for class jahuwaldt.aero.ConicalShock
Construct a conical shock solver that assumes the gas properties for air (gamma = 1.4).
ConicalShock(double) - Constructor for class jahuwaldt.aero.ConicalShock
Construct a conical shock solver object using the specified specific heat ratio for the gas that the shock is in (use 1.4 for air).
contains(FloatTable) - Method in class jahuwaldt.tools.tables.FTableDatabase
Tests to see if the specified table object is contained in this database.
containsName(String) - Method in class jahuwaldt.tools.tables.FTableDatabase
Tests to see if a table exists in the database with the specified name.
ControlAero3DOF - Interface in jahuwaldt.aero
Interface in common to all 3-DOF static flight control aerodynamics models.
ControlAero3DOFTabular - Class in jahuwaldt.aero
A 3DOF aerodynamic model of flight control deflection that makes use of data tabulated as a function of angle of attack, Mach number, and control deflection angle.
ControlAero3DOFTabular(FloatTable, FloatTable, FloatTable, String, String, String) - Constructor for class jahuwaldt.aero.ControlAero3DOFTabular
Construct a tabular 3-DOF aerodynamics control surface model.
ControlHingeMoments - Interface in jahuwaldt.aero
Interface in common to all aerodynamic flight control hinge-moment models.
ControlHMLinearizedTabular - Class in jahuwaldt.aero
A model of flight control surface aerodynamic hinge-moments that makes use of a linearized component build-up where each component is data tabulated as a function of Mach number.
ControlHMLinearizedTabular(FloatTable, FloatTable, FloatTable, String) - Constructor for class jahuwaldt.aero.ControlHMLinearizedTabular
Construct a linearized, tabular control surface aerodynamic hinge-moment model.
cosA - Variable in class jahuwaldt.aero.Aero3DOFTabular
The cosine of angle of attack.
create(String, double) - Static method in class jahuwaldt.aero.airfoils.NACAFactory
Returns an Airfoil object corresponding to the airfoil designation sting passed in.
cs - Variable in class jahuwaldt.aero.StdAtmos
 
CSVReader - Class in jahuwaldt.tools.tables
A class that provides a method for reading or writing a specially organized CSV (Comma-Separated-Value) multi-table file.
CSVReader() - Constructor for class jahuwaldt.tools.tables.CSVReader
 
CYb - Variable in class jahuwaldt.aero.AeroCoefficients
Body axes force coefficients.
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