- 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.