- P0() - Method in class jahuwaldt.aero.StdAtmos
-
Returns the standard sea level pressure for this
atmosphere model.
- P0() - Method in class jahuwaldt.aero.StdAtmos1962
-
Returns the standard sea level pressure for this
atmosphere model.
- P0() - Method in class jahuwaldt.aero.StdAtmos1976
-
Returns the standard sea level pressure for this
atmosphere model in Newtons/m^2.
- P2_P1(double, double) - Static method in class jahuwaldt.aero.Isentropic
-
Calculate the isentropic pressure ratio between two points in the flow given the
temperature ratio.
- panels() - Method in class jahuwaldt.aero.panelgeom.GeomNetwork
-
Return an iteration of all the panels in this network.
- parse(String, ParsePosition) - Method in class jahuwaldt.util.ExponentialFormat
-
Returns an instance of Number with a value matching the given string.
- parse(String, ParsePosition) - Method in class jahuwaldt.util.GeneralFormat
-
Returns an instance of Number with a value matching the given string.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA63ASeries
-
Fill in phi, eps vectors for 63A series airfoil.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA63Series
-
Fill in phi, eps vectors for 63 series airfoil.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA64ASeries
-
Fill in phi, eps vectors for 64A series airfoil.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA64Series
-
Fill in phi, eps vectors for 64 series airfoil.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA65ASeries
-
Fill in phi, eps vectors for 65A series airfoil.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA65Series
-
Fill in phi, eps vectors for 65 series airfoil.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA66Series
-
Fill in phi, eps vectors for 66 series airfoil.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA67Series
-
Fill in phi, eps vectors for 67 series airfoil.
- phep(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA6Series
-
Fill in phi, eps vectors for 63 series airfoil.
- phi - Variable in class jahuwaldt.aero.AeroCoefficients
-
Flow angles used to transform between axis systems.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA63ASeries
-
Fill in the psi vector for a 63A series airfoil.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA63Series
-
Fill in the psi vector for a 63 series airfoil.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA64ASeries
-
Fill in the psi vector for a 64A series airfoil.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA64Series
-
Fill in the psi vector for a 64 series airfoil.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA65ASeries
-
Fill in the psi vector for a 65A series airfoil.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA65Series
-
Fill in the psi vector for a 65 series airfoil.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA66Series
-
Fill in the psi vector for a 66 series airfoil.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA67Series
-
Fill in the psi vector for a 67 series airfoil.
- phps(double[], double[]) - Method in class jahuwaldt.aero.airfoils.NACA6Series
-
Fill in the psi vector for a 63 series airfoil.
- pm_func(double, double) - Static method in class jahuwaldt.aero.ShockMethods
-
Calculates the Prandtl-Meyer function (nu) for a
calorically perfect gas.
- pm_Mach(double, double, double) - Static method in class jahuwaldt.aero.ShockMethods
-
Back solves the Prandtl-Meyer function (nu) for Mach
number.
- pm_Mach(double, double, double, ShockMachNuEvaluator) - Static method in class jahuwaldt.aero.ShockMethods
-
Back solves the Prandtl-Meyer function (nu) for Mach
number.
- POI_TYPE - Static variable in class jahuwaldt.aero.panelgeom.GeomReaderFactory
-
Type identifier for a POI ($POINTS) A502/A633 geometry input file.
- POIGeomReader - Class in jahuwaldt.aero.panelgeom
-
A class for reading vehicle geometry from a POINTS (POI)
formatted geometry file.
- POIGeomReader() - Constructor for class jahuwaldt.aero.panelgeom.POIGeomReader
-
- pos - Variable in class jahuwaldt.tools.tables.FloatTable
-
- POSTTableReader - Class in jahuwaldt.tools.tables
-
A class that provides methods for reading
or writing a POST table (*.dat) formatted multi-table file.
- POSTTableReader() - Constructor for class jahuwaldt.tools.tables.POSTTableReader
-
- prandtlGlauert(double, double) - Static method in class jahuwaldt.aero.AeroMethods
-
Prandtl-Glauert compressibility correction.
- PT_P(double, double) - Static method in class jahuwaldt.aero.Isentropic
-
Calculates the ratio of total to static pressure at a point in a flow as a function
of Mach number at that point.
- put(FloatTable) - Method in class jahuwaldt.tools.tables.FTableDatabase
-
Add the specified table to this database.
- putAll(FTableDatabase) - Method in class jahuwaldt.tools.tables.FTableDatabase
-
Add the contents of the specified table database to this database.
- putData(Object, Object) - Method in interface jahuwaldt.aero.panelgeom.GeomElement
-
Store application specific data that can be assigned to this geometry element.
- putData(Object, Object) - Method in class jahuwaldt.aero.panelgeom.GeomElementList
-
Store application specific data that can be assigned to this geometry element.
- putData(Object, Object) - Method in class jahuwaldt.aero.panelgeom.GeomNetwork
-
Store application specific data that can be assigned to this network.