- read(InputStream, String) - Method in interface jahuwaldt.aero.panelgeom.GeomReader
-
Method provided by sub-classes that reads in a geometry file from the supplied
input stream and returns a properly formatted configuration geometry object that
contains the geometry from the file.
- read(InputStream, String) - Method in class jahuwaldt.aero.panelgeom.GGPGeomReader
-
Method that reads in a GGP formatted geometry file from the specified input stream
and returns a configuration geometry object that contains the geometry from the GGP
file.
- read(InputStream, String) - Method in class jahuwaldt.aero.panelgeom.POIGeomReader
-
Method that reads in a POINTS (POI) geometry file from the
specified input stream and returns a configuration geometry
object that contains the geometry from the POI file.
- read(InputStream) - Method in class jahuwaldt.tools.tables.C81Reader
-
Method that reads in C-81 airfoil aerodynamics formatted data
from the specified input stream and returns that data as an
FTableDatabase object.
- read(InputStream) - Method in class jahuwaldt.tools.tables.CSVReader
-
Method that reads in specially organized CSV formatted data
from the specified input stream and returns that data as an
FTableDatabase object.
- read(InputStream) - Method in class jahuwaldt.tools.tables.FDAReader
-
Method that reads in Functional Data Handling ASCII system (FDA)
formatted data from the specified input stream and returns that data as an
FTableDatabase object.
- read(InputStream) - Method in class jahuwaldt.tools.tables.FLABSavReader
-
Method that reads in ART FlightLab SAV formatted data
from the specified input stream and returns that data as an
FTableDatabase object.
- read(InputStream) - Method in interface jahuwaldt.tools.tables.FTableReader
-
Interface for reading in data from an input stream
and returning that data as a list of DataSet objects.
- read(InputStream) - Method in class jahuwaldt.tools.tables.NASAReader
-
Method that reads in NASA 2,3, or 4 argument table formatted data
from the specified input stream and returns that data as an
FTableDatabase object.
- read(InputStream) - Method in class jahuwaldt.tools.tables.OTISTableReader
-
Method that reads in OTIS table formatted data
from the specified input stream and returns that data as an
FTableDatabase object.
- read(InputStream) - Method in class jahuwaldt.tools.tables.POSTTableReader
-
Method that reads in POST table formatted data
from the specified input stream and returns that data as an
FTableDatabase object.
- readNetwork(LineNumberReader) - Method in class jahuwaldt.aero.panelgeom.POIGeomReader
-
Reads a single network from an input stream (pointing to a POI file).
- ref - Variable in class jahuwaldt.aero.AeroCoefficients
-
Aerodynamic reference quantities are stored here.
- remove(int) - Method in class jahuwaldt.aero.panelgeom.GeomElementList
-
Remove the sub-element at the specified position in this geometry element.
- remove(String) - Method in class jahuwaldt.tools.tables.FTableDatabase
-
Remove the named table from this database.
- removeNote(int) - Method in class jahuwaldt.tools.tables.FloatTable
-
Remove a specified note String from the list of notes
associated with this table.
- removeNote(int) - Method in class jahuwaldt.tools.tables.FTableDatabase
-
Remove a specified note String from the list of notes
associated with this table database.
- RHO0() - Method in class jahuwaldt.aero.StdAtmos
-
Returns the standard sea level density for this
atmosphere model.
- RHO0() - Method in class jahuwaldt.aero.StdAtmos1962
-
Returns the standard sea level density for this
atmosphere model.
- RHO0() - Method in class jahuwaldt.aero.StdAtmos1976
-
Returns the standard sea level density for this
atmosphere model in kg/L (g/cm^3).
- rho2_rho1(double, double) - Static method in class jahuwaldt.aero.Isentropic
-
Calculate the isentropic density ratio between two points in the flow given the
temperature ratio.
- rhoT_rho(double, double) - Static method in class jahuwaldt.aero.Isentropic
-
Calculates the ratio of total to static density at a point in a flow as a function
of Mach number at that point.
- RLE - Variable in class jahuwaldt.aero.airfoils.NACA4ModUncambered
-
The leading edge radius in percent chord length.