- 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.