- M_fn_delta_VC(double, double, double) - Static method in class jahuwaldt.aero.Airspeeds
-
Method that calculates Mach number as a function of pressure ratio, and calibrated
airspeed.
- M_fn_VT_a(double, double) - Static method in class jahuwaldt.aero.Airspeeds
-
Calculates the Mach number as a function of the true airspeed and local speed of
sound.
- machAngle(double) - Static method in class jahuwaldt.aero.ShockMethods
-
Calculates the angle of a Mach wave with respect
to the direction of motion (Mach angle).
- main(String[]) - Static method in class jahuwaldt.aero.AeroCoefXAft
-
A simple method to test the methods in this class.
- main(String[]) - Static method in class jahuwaldt.aero.AeroMethods
-
A simple method to test the methods in this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA4Cambered
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA4ModCambered
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA4ModUncambered
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA4Uncambered
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA5Cambered
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA5Reflexed
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA63ASeries
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA63Series
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA64ASeries
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA64Series
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA65ASeries
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA65Series
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA66Series
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACA67Series
-
Simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.airfoils.NACAFactory
-
A simple method to test this class.
- main(String[]) - Static method in class jahuwaldt.aero.ConicalShock
-
A simple method to test the methods in this class.
- main(String[]) - Static method in class jahuwaldt.aero.Isentropic
-
A simple method to test the isentropic methods in this class.
- main(String[]) - Static method in class jahuwaldt.aero.ShockMethods
-
A simple method to test the shock methods in this
class.
- main(String[]) - Static method in class jahuwaldt.aero.StdAtmos1962
-
A simple method to test the 1962 standard atmosphere.
- main(String[]) - Static method in class jahuwaldt.aero.StdAtmos1976
-
A simple method to test the 1976 standard atmosphere.
- main(String[]) - Static method in class jahuwaldt.util.ExponentialFormat
-
A simple static method to test this class.
- main(String[]) - Static method in class jahuwaldt.util.GeneralFormat
-
A simple static method to test this class.
- maxAltitude() - Method in class jahuwaldt.aero.StdAtmos
-
Returns the maximum altitude supported by this
atmosphere model.
- maxAltitude() - Method in class jahuwaldt.aero.StdAtmos1962
-
Returns the maximum altitude supported by this
atmosphere model.
- maxAltitude() - Method in class jahuwaldt.aero.StdAtmos1976
-
Returns the maximum altitude supported by this
atmosphere model in meters.
- MAYBE - Static variable in interface jahuwaldt.tools.tables.FTableReader
-
Constant indicating that a reader might be able to read a specified file,
but can't determine for sure.
- Mcr(double, double, double) - Static method in class jahuwaldt.aero.AeroMethods
-
Estimates the critical Mach number given the minimum
incompressible pressure coefficient.
- Me(double, double, double, boolean) - Static method in class jahuwaldt.aero.Isentropic
-
Calculates the Mach number at the entrance or exit of a duct (nozzle) given the
ratio of the local duct area at the entrance or exit to the area where the sonic
(M=1) condition exists.
- Me(double, double, double, boolean, IsentropicMeEvaluator) - Static method in class jahuwaldt.aero.Isentropic
-
Calculates the Mach number at the entrance or exit of a duct (nozzle) given the
ratio of the local duct area at the entrance or exit to the area where the sonic
(M=1) condition exists.
- minAltitude() - Method in class jahuwaldt.aero.StdAtmos
-
Returns the minimum altitude supported by this
atmosphere model.
- minAltitude() - Method in class jahuwaldt.aero.StdAtmos1962
-
Returns the minimum altitude supported by this
atmosphere model.
- minAltitude() - Method in class jahuwaldt.aero.StdAtmos1976
-
Returns the minimum altitude supported by this
atmosphere model in meters.
- modCamberLine(double, boolean, double, double, double, double, double[]) - Method in class jahuwaldt.aero.airfoils.NACA6ASeries
-
Method used by 6*A series airfoils to modify the camber line.
- modCamberLine(double, boolean, double, double, double, double, double[]) - Method in class jahuwaldt.aero.airfoils.NACA6Series
-
Method used by 6*A series airfoils to modify the camber line.
- modTrailingEdge(double, double, double, double, double, double[]) - Method in class jahuwaldt.aero.airfoils.NACA6ASeries
-
Method used by 6*A series airfoils to modify the airfoil trailing edge.
- modTrailingEdge(double, double, double, double, double, double[]) - Method in class jahuwaldt.aero.airfoils.NACA6Series
-
Method used by 6*A series airfoils to modify the airfoil trailing edge.