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T

T0() - Method in class jahuwaldt.aero.StdAtmos
Returns the standard sea level temperature for this atmosphere model.
T0() - Method in class jahuwaldt.aero.StdAtmos1962
Returns the standard sea level temperature for this atmosphere model.
T0() - Method in class jahuwaldt.aero.StdAtmos1976
Returns the standard sea level temperature for this atmosphere model in Kelvin.
T2_T1(double, double) - Static method in class jahuwaldt.aero.Isentropic
Calculate the isentropic temperature ratio between two points in the flow given the pressure ratio.
tanth - Variable in class jahuwaldt.aero.airfoils.NACA4Uncambered.Ordinate
The tangent of the local surface angle due to camber.
tblName - Variable in class jahuwaldt.tools.tables.FloatTable
The name of this data table.
theta - Variable in class jahuwaldt.aero.StdAtmos
 
thp - Variable in class jahuwaldt.aero.airfoils.NACA4Uncambered.Ordinate
The local surface angle due to camber.
toArray() - Method in class jahuwaldt.tools.tables.FTableDatabase
Return the contents of this table database as an array of FloatTable objects.
TOC - Variable in class jahuwaldt.aero.airfoils.NACA4Uncambered
Thickness-to-Chord Ratio
toString() - Method in class jahuwaldt.aero.Aero3DOFTabular
Return a string representation of this object.
toString() - Method in class jahuwaldt.aero.Aero3DOFTabularGE
Return a string representation of this object.
toString() - Method in class jahuwaldt.aero.AeroReference
Method that returns a string representations of the reference quantities contained in this object.
toString() - Method in class jahuwaldt.aero.airfoils.NACA4Cambered
Returns a string representation of this airfoil (the NACA designation of this airfoil).
toString() - Method in class jahuwaldt.aero.airfoils.NACA4ModCambered
Returns a string representation of this airfoil (the NACA designation of this airfoil).
toString() - Method in class jahuwaldt.aero.airfoils.NACA4ModUncambered
Returns a string representation of this airfoil (the NACA designation of this airfoil).
toString() - Method in class jahuwaldt.aero.airfoils.NACA4Uncambered
Returns a string representation of this airfoil (the NACA designation of this airfoil).
toString() - Method in class jahuwaldt.aero.airfoils.NACA5Cambered
Returns a string representation of this airfoil (the NACA designation of this airfoil).
toString() - Method in class jahuwaldt.aero.airfoils.NACA5Reflexed
Returns a string representation of this airfoil (the NACA designation of this airfoil).
toString() - Method in class jahuwaldt.aero.airfoils.NACA6Series
Returns a string representation of this airfoil (the NACA designation of this airfoil).
toString() - Method in class jahuwaldt.aero.ControlAero3DOFTabular
Return a string representation of this object.
toString() - Method in class jahuwaldt.aero.ControlHMLinearizedTabular
Return a string representation of this object.
toString() - Method in class jahuwaldt.aero.panelgeom.GeomElementList
Create a string representation of this geometry element by outputting the element's name and it's bounding rectangle coordinates.
toString() - Method in class jahuwaldt.aero.panelgeom.GeomNetwork
Create a string representation of this network by outputing the network name and it's bounding rectangle coordinates.
toString() - Method in class jahuwaldt.aero.panelgeom.GeomPanel
Create a string representation of this panel by outputting the panel centroid location.
toString() - Method in class jahuwaldt.aero.panelgeom.GeomPoint
Creates a string representation of this point by simply outputting the X,Y,Z coordinates of the point.
toString() - Method in class jahuwaldt.aero.StdAtmos
Creates a String representation of this object.
toString() - Method in class jahuwaldt.tools.tables.C81Reader
Returns a string representation of the object.
toString() - Method in class jahuwaldt.tools.tables.CSVReader
Returns a string representation of the object.
toString() - Method in class jahuwaldt.tools.tables.FDAReader
Returns a string representation of the object.
toString() - Method in class jahuwaldt.tools.tables.FLABSavReader
Returns a string representation of the object.
toString() - Method in class jahuwaldt.tools.tables.FloatTable
Output the name of the table and the names of it's independent variables.
toString() - Method in class jahuwaldt.tools.tables.FTableDatabase
Returns a String representation of this FTableDatabase object.
toString() - Method in class jahuwaldt.tools.tables.NASAReader
Returns a string representation of the object.
toString() - Method in class jahuwaldt.tools.tables.OTISTableReader
Returns a string representation of the object.
toString() - Method in class jahuwaldt.tools.tables.POSTTableReader
Returns a string representation of the object.
ToStringComparator<T> - Class in jahuwaldt.util
A comparator that lexicographically compares objects based on the value returned by each object's "toString()" method.
ToStringComparator() - Constructor for class jahuwaldt.util.ToStringComparator
 
translate(double, double, double) - Method in interface jahuwaldt.aero.panelgeom.GeomElement
Translate this element by an incremental amount along each axis.
translate(double, double, double) - Method in class jahuwaldt.aero.panelgeom.GeomElementList
Translate this element by an incremental amount along each axis.
translate(double, double, double) - Method in class jahuwaldt.aero.panelgeom.GeomNetwork
Translate this network by an incremental amount along each axis.
translate(double, double, double) - Method in class jahuwaldt.aero.panelgeom.GeomPanel
Translate this panel by an incremental amount along each axis.
translate(double, double, double) - Method in class jahuwaldt.aero.panelgeom.GeomPoint
Translate this point by an incremental amount along each axis.
TRUtils - Class in jahuwaldt.tools.tables
A collection of static methods that are useful for TableReader objects to use.
TRUtils() - Constructor for class jahuwaldt.tools.tables.TRUtils
 
TT_T(double, double) - Static method in class jahuwaldt.aero.Isentropic
Calculates the ratio of total to static temperature at a point in a flow as a function of Mach number at that point.
turbSkinFriction(double, double, double) - Static method in class jahuwaldt.aero.AeroMethods
Function that calculates the turbulent skin friction coefficient in a boundary layer including the effects of compressibility, viscosity, and heat transfer.
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